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	<title>NASASpaceFlight.com &#187; Unmanned</title>
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		<title>SpaceX to launch two AsiaSat satellites via Falcon 9 in 2014</title>
		<link>http://www.nasaspaceflight.com/2012/02/spacex-launch-two-asiasat-satellites-falcon-9-2014/</link>
		<comments>http://www.nasaspaceflight.com/2012/02/spacex-launch-two-asiasat-satellites-falcon-9-2014/#comments</comments>
		<pubDate>Wed, 08 Feb 2012 16:14:08 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
				<category><![CDATA[Commercial]]></category>
		<category><![CDATA[Unmanned]]></category>

		<guid isPermaLink="false">http://www.nasaspaceflight.com/?p=23074</guid>
		<description><![CDATA[SpaceX have announced a contract to launch two Asia Satellite Telecommunications Company Limited (AsiaSat) satellites. AsiaSat 6 and AsiaSat 8 will be launched via SpaceX&#8217;s Falcon 9 launch vehicle, after the previous two AsiaSats were launched via the Russian Proton rocket, under the control of International Launch Services (ILS). SpaceX AsiaSat Win: Wednesday&#8217;s contract announcement to launch [...]


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			<content:encoded><![CDATA[<p>SpaceX have announced a contract to launch two Asia Satellite Telecommunications Company Limited (AsiaSat) satellites. AsiaSat 6 and AsiaSat 8 will be launched via SpaceX&#8217;s Falcon 9 launch vehicle, after the previous two AsiaSats were launched via the Russian Proton rocket, under the control of International Launch Services (ILS).</p>
<p><span id="more-23074"></span><strong>SpaceX AsiaSat Win:</strong></p>
<p>Wednesday&#8217;s contract announcement to launch the AsiaSat birds has resulted in SpaceX&#8217;s order book now being filled by a majority of commercial missions. The balance is concentrated on NASA contracts, as <a href="http://www.nasaspaceflight.com/2012/01/dragon-slips-spacex-determined-return-us-crewed-access-leo/" target="_blank">SpaceX push towards their commercial resupply (CRS) of the International Space Station</a> (ISS).</p>
<p>The California-based company is <a href="http://www.nasaspaceflight.com/tag/spacex/" target="_blank">also pushing towards the development of a crewed capability to return US domestic access to Low Earth Orbit</a>.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z37.jpg"><img class="alignleft size-full wp-image-23076" title="Z3" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z37.jpg" alt="" width="351" height="238" /></a>The AsiaSat launches will be conducted by the Falcon 9 launch vehicle, lifting off from Florida&#8217;s Cape Canaveral Air Force Station (CCAFS) Launch Complex 40 in the first quarter of 2014.</p>
<p>&#8220;SpaceX is proud to be the choice of AsiaSat, a pioneer in advancing satellite communications in Asia,&#8221; said Elon Musk, SpaceX CEO and Chief Technology Officer.</p>
<p>&#8220;We are producing the most advanced launch vehicles in the world, and the international launch market has responded &#8211; commercial launches now represent over 60 percent of our upcoming missions.&#8221;</p>
<p>AsiaSat is the leading satellite broadcasting and telecommunications in Asia Pacific, opening their operations with AsiaSat 1 &#8211; Asia&#8217;s first privately owned regional satellite &#8211; in April 1990.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z341.jpg"><img class="alignleft size-full wp-image-23077" title="Z34" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z341.jpg" alt="" width="350" height="225" /></a>However, AsiaSat-1&#8242;s history began under the call sign of WeStar 6, launched in the payload bay of Space Shuttle Challenger during her STS-41B mission.</p>
<p><a href="http://www.nasaspaceflight.com/2011/01/1983-1986-missions-history-space-shuttle-challenger/" target="_blank">Challenger lifted off at 08:00 EST on February 3, 1984, on her fourth launch to begin the 10th Space Shuttle mission</a> and the first under the new flight classification system. Had the previous numerical designation continued, this would have been the STS-11 mission.</p>
<p>Like her three previous missions, Challenger was inserted into a 28.5 degree 189nm orbit.</p>
<p>Once in orbit, Challenger&#8217;s crew deployed the WeStar 6 and Palapa-B2 satellites, while Bruce McCandless and Robert L. Stewart performed the first untethered EVA in history using the Manned Maneuvering Unit (McCandless) and the SRMS foot restraint for EVA purposes (Stewart).</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?board=45.0">SpaceX Forum Section</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?action=tags&amp;tags=SpaceX">L2 SpaceX Section</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=34.0">L2 Historical Section</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div>
<p>Also carried aboard Challenger on this flight was the German-built Shuttle Pallet Satellite &#8211; which became the first satellite to be refurbished and re-flown into space following its first flight on STS-7. An electrical problem with SRMS (Shuttle Remote Manipulator System), however, precluded the deployment of the satellite as intended.</p>
<p>Sadly, WeStar 6 &#8211; and Palapa-B2 &#8211; became a black mark on the mission, after the satellites failed to properly fire their PAMs (Payload Assist Motor) after deployment, meaning they could not reach its desired GeoStationary orbit, and were stranded in a useless LEO trajectory.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z55.jpg"><img class="alignleft size-full wp-image-23078" title="Z5" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z55.jpg" alt="" width="349" height="251" /></a>Later that year, <a href="http://www.nasaspaceflight.com/2011/02/workhorse-discovery-stands-ready-for-final-mission/" target="_blank">Discovery came to the rescue, undertaking her second mission, STS-51A</a>.</p>
<p>This mission, which launched on November 8, 1984, marked the first time a Shuttle orbiter deployed two communications satellites and retrieved from orbit two other communications satellites.</p>
<p>The retrieval of the WeStar 6 and Palapa-B2 communications satellites also marked the last untethered spacewalk of the Shuttle Program until 1994.</p>
<p>Brought back down to Earth and refurbished, AsiaSat purchased the WeStar 6 satellite and relaunched it as AsiaSat 1 on a Chinese Long March 3 rocket in 1990. This satellite is no longer in service.</p>
<p>AsiaSat currently owns and operates four satellites AsiaSat 3S, AsiaSat 4, AsiaSat 5 and AsiaSat 7 &#8211; which are designed to deliver excellent performance, coverage and connectivity across the Asia-Pacific region.</p>
<p><a href="http://www.nasaspaceflight.com/2009/08/ils-proton-m-launches-with-asiasat-5/" target="_blank">AsiaSat 5 &#8211; launched in August, 2009 via an ILS Proton-M</a> &#8211; was placed into orbit as a new generation satellite equipped with the latest technology and new beam coverage to provide highest quality television broadcast, telephone networks and VSAT networks for broadband multimedia services across Asia Pacific.</p>
<p>In addition to a very powerful pan-Asian C-band footprint and the improved Ku-band East Asia beam, AsiaSat 5′s Ku-band South Asia and in-orbit steerable beams were designed to serve new market requirements and to offer full backup capability in network coverage with AsiaSat&#8217;s existing satellites AsiaSat 3S and AsiaSat 4. AsiaSat 5 replaced AsiaSat 2 at 100.5 degrees East.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z66.jpg"><img class="alignleft size-full wp-image-23079" title="Z6" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z66.jpg" alt="" width="348" height="247" /></a>AsiaSat 7 was designed as a replacement satellite for AsiaSat 3S at 105.5 degrees East. This new generation satellite sports 28 C-band and 17 Ku-band transponders as well as a Ka-band payload. Its region-wide C-band beam covers over 50 countries across Asia, the Middle East, Australasia and Central Asia.</p>
<p>AsiaSat 7 also offers 3 Ku-band beams with intra beam switching capability, serving East Asia and South Asia, and a steerable Ku beam. AsiaSat 7 is providing satellite capacity for television broadcast and VSAT Network services across the Asia-Pacific Region.</p>
<p>The 3,813 kg (8,406 lbs) satellite was built by Space Systems/Loral and is expected to enjoy 15 years of service in orbit.</p>
<p><a href="http://www.nasaspaceflight.com/2011/11/ils-proton-m-launch-asiasat-7/" target="_blank">The launch, conducted from the Baikonur Cosmodrome in Kazakhstan on November 25, 2011 &#8211; was also an ILS mission, utilizing the Russian Proton-M launch vehicle</a>. With the task of lofting AsiaSat 6 and 8 into orbit to be conducted by Falcon 9, the contract announcement appears to be a victory for SpaceX in the competitive launch services market.</p>
<p>&#8220;We are pleased to have SpaceX as our launch partner for the two upcoming missions. We look forward to the timely and successful launches of AsiaSat 6 and AsiaSat 8, thereby expanding our fleet from four to six satellites in 2014 to provide more high quality and comprehensive satellite services in the Asia-Pacific region,&#8221; said William Wade, President and Chief Executive Officer of AsiaSat.</p>
<p>AsiaSat 6 will have 28 high-powered C-band transponders while AsiaSat 8 will have 24 Ku-band transponders and a Ka-band beam. The high-powered transponders on the satellite will enable the use of small antennas on the ground.</p>
<p>The two SS/L 1300 satellites will serve Asia, the Middle East and Australasia.</p>
<p>(Images via SpaceX, ILS, NASA, and L2)</p>
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		<title>Aerojet&#8217;s confidence in Next Generation Engine and green propellants</title>
		<link>http://www.nasaspaceflight.com/2012/02/aerojets-confidence-next-generation-engine-green-propellants/</link>
		<comments>http://www.nasaspaceflight.com/2012/02/aerojets-confidence-next-generation-engine-green-propellants/#comments</comments>
		<pubDate>Tue, 07 Feb 2012 03:59:15 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
				<category><![CDATA[Commercial]]></category>
		<category><![CDATA[Featured]]></category>
		<category><![CDATA[Unmanned]]></category>
		<category><![CDATA[Aerojet]]></category>
		<category><![CDATA[Monopropellants]]></category>
		<category><![CDATA[NGE]]></category>

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		<description><![CDATA[Californian aerospace company Aerojet believe they are in a good position to continue their advancements in the development of rocket engines, ranging from the Next Generation Engine (NGE) for the US Air Force&#8217;s Evolved Expendable Launch Vehicle (EELV) program, through to environmentally &#8220;green&#8221; propellants for propulsion hardware. Aerojet Engine Development: While Aerojet are already involved [...]


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			<content:encoded><![CDATA[<p>Californian aerospace company Aerojet believe they are in a good position to continue their advancements in the development of rocket engines, ranging from the Next Generation Engine (NGE) for the US Air Force&#8217;s Evolved Expendable Launch Vehicle (EELV) program, through to environmentally &#8220;green&#8221; propellants for propulsion hardware.</p>
<p><span id="more-23038"></span><strong>Aerojet Engine Development:</strong></p>
<p><a href="http://www.nasaspaceflight.com/2012/01/aerojet-solar-electric-propulsion-enabler-exploration-gateway/" target="_blank">While Aerojet are already involved in a wide range of propulsive requirements for launch vehicles and spacecraft</a>, work is already well under way for their effort to become the provider of the Next Generation Engine (NGE), a process started via the Air Force&#8217;s Request For Information (RFI) over a year ago.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z35.jpg"><img class="alignleft size-full wp-image-23041" title="Z3" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z35.jpg" alt="" width="350" height="263" /></a>The RFI noted it was seeking an Upper Stage engine utilizing modern design and manufacturing methods, while it would be expected that the new engine will demonstrate state-of-the-art operating margin and reliability and minimize life-cycle costs, with an aim of replacing the RL-10 &#8211; which is used in various forms with <a href="http://www.nasaspaceflight.com/2011/11/the-respected-atlas-v-making-early-strides-transition/" target="_blank">Atlas&#8217; Centaur Upper Stage (RL-10A-3)</a> and <a href="http://www.nasaspaceflight.com/tag/delta-iv/" target="_blank">Delta IV&#8217;s Upper Stage (RL-10B-2).<br />
</a><br />
Aerojet recently noted they had successfully completed a major milestone in the development of a ground demonstrator for the Next Generation Engine (NGE) program, <a href="http://www.nasaspaceflight.com/2011/11/aerojet-complete-pdr-next-gen-upper-stage-engine-turbopump/" target="_blank">announcing the completion of the Preliminary Design Review (PDR) of the turbopump assembly</a>.</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?board=13.0">US Launchers Section</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=48.0">L2 SLS Section</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=29.0">L2 Future Spacecraft Section</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div>
<p>The engine under development &#8211; which is yet to receive a name &#8211; would not be restricted to just US Air Force/EELV use, according to Julie Van Kleeck, Aerojet Vice President, Space &amp; Launch System speaking in an interview with NASASpaceflight.com.</p>
<p>&#8220;For now we are assuming the RL-10 engine requirements with additional consideration of the requirements put forth in the AF September 2010 RFI. (Next Generation Engine (NGE) Request for Information; Solicitation Number: SMC10-55; Agency: Department of the Air Force; Office: Air Force Space Command; Location: SMC &#8211; Space and Missile Systems Center).</p>
<p>&#8220;We do believe this engine can serve future civil as well as Air Force needs.&#8221;</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/F25.jpg"><img class="alignleft size-full wp-image-23042" title="F25" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/F25.jpg" alt="" width="347" height="264" /></a>Aerojet &#8211; who previously noted it has been decades since there has been an open engine competition in the United States &#8211; added they are unable to compare their new engine to an RL-10 derivative at this stage. However, they are confident they can present their NGE as a major step forward.</p>
<p>&#8220;We don&#8217;t know many specifics about RL-10 derivatives since little has been made public. Aerojet believes that our offering for NGE will make major improvements over the current RL-10 in cost and reliability and have equal or greater performance depending on configuration,&#8221; added Ms Van Kleeck.</p>
<p>The Californian-based company are involved in a number of future engine projects, <a href="http://www.nasaspaceflight.com/tag/hlv/" target="_blank">not least the advanced booster for the Space Launch System</a> (SLS), but also in the field of environmentally &#8220;green&#8221; engines.</p>
<p>With experience in working with Hydroxylammonium nitrate or hydroxylamine nitrate (HAN) powered engines for uncrewed spacecraft, Aerojet noted they are also working on a nitrous-ethanol bipropellant system for Human Space Flight applications.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z91.jpg"><img class="alignleft size-full wp-image-23046" title="Z9" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z91.jpg" alt="" width="350" height="196" /></a>&#8220;While Aerojet has been developing HAN-based monopropellants for a wide range of applications since 1990, Human Spaceflight is not a current focus for this effort. For HSF, our current green propulsion focus is a nitrous-ethanol bipropellant system,&#8221; noted Ms Van Kleeck.</p>
<p>It has been publicly known that HAN is being developed as a potential propellant for launch vehicles, both in the solid form as a solid propellant oxidizer, and in the aqueous solution in monopropellant rockets.</p>
<p>According to technical papers &#8211; such as those associated with the US Department of Energy &#8211; it is typically bonded with glycidyl azide polymer (GAP), Hydroxyl-terminated polybutadiene (HTPB), or carboxy-terminated polybutadiene (CTPB). The catalyst is a noble metal, similar to the other monopropellants that use silver or palladium.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z45.jpg"><img class="alignleft size-full wp-image-23043" title="Z4" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z45.jpg" alt="" width="287" height="224" /></a>&#8220;For the HAN-monopropellant systems we are currently focused on robotic spacecraft and defense applications,&#8221; Ms Van Kleeck continued. &#8220;Aerojet has successfully tested HAN thrusters from 0.2 lbf up to 150 lbf and has found no limitations to developing even higher thrust engines. When developing new, green propellants, one needs to consider both environmental and safety issues.</p>
<p>&#8220;For HSF, if green monopropellants become attractive, Aerojet believes that HAN is the leading green monopropellant candidate if you consider all of the safety and handling issues.&#8221;</p>
<p>As aforementioned, Ms Van Kleeck noted that Aerojet place a large amount of consideration on both the environmental and safety elements of their advanced propellants, not least their impact on humans, but also for the atmosphere of Mars.</p>
<p>&#8220;Aerojet has developed both monopropellant and bipropellant liquid rocket engines that utilize environmentally friendly propellants. Our monopropellant efforts include HAN based engines and Nitrous Oxide based engines. In the bipropellant arena, we have developed Nitrous-Ethanol, LOX/Methane, LOX/Hydrogen and LOX/Ethanol engines,&#8221; added Ms Van Kleeck.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z64.jpg"><img class="alignleft size-full wp-image-23044" title="Z6" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/02/Z64.jpg" alt="" width="349" height="242" /></a>&#8220;<a href="http://www.nasaspaceflight.com/2011/11/live-atlas-v-launch-nasas-msl-rover-mars/">For interplanetary missions to Mars</a>, NASA has chosen Aerojet&#8217;s monopropellant hydrazine thrusters for both cruise and landing for all Mars landers to date for the simple reason that hydrazine (N2H4) does not contain carbon.</p>
<p>&#8220;For all advanced propellants, both environmental and safety considerations are very important, and our selections are based on a balance of both of these critical factors. Insofar as toxicity to humans, we have done extensive work on our selected propellants and have found that they meet our requirements.</p>
<p>&#8220;Just as important, extensive testing has shown that our propellants are the safest to handle and use in typical test and operational settings.&#8221;</p>
<p>(Images: Via NASA, ACS.org and Aerojet.)</p>
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		<title>No impact to two ULA missions following Delta Mariner accident</title>
		<link>http://www.nasaspaceflight.com/2012/01/no-impact-ula-missions-delta-mariner-accident/</link>
		<comments>http://www.nasaspaceflight.com/2012/01/no-impact-ula-missions-delta-mariner-accident/#comments</comments>
		<pubDate>Sat, 28 Jan 2012 22:16:06 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
				<category><![CDATA[Unmanned]]></category>
		<category><![CDATA[Atlas V]]></category>
		<category><![CDATA[Delta]]></category>
		<category><![CDATA[ULA]]></category>

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		<description><![CDATA[The Delta Mariner &#8211; carrying hardware elements targeting two future launches &#8211; collided with the Eggner&#8217;s Ferry Bridge over Kentucky Lake on Thursday night. However, despite extensive damage to the bridge, no serious injuries were reported. ULA have noted that there will be no mission impact to the Advanced Extremely High Frequency (AEHF-2) and Radiation [...]


Related posts:<ol><li><a href='http://www.nasaspaceflight.com/2009/03/live-delta-ii-launch-penultimate-gps-iir-satellite-2/' rel='bookmark' title='Permanent Link: Delta II launches penultimate GPS-IIR satellite'>Delta II launches penultimate GPS-IIR satellite</a> <small>A United Launch Alliance (ULA) Delta II rocket has launched this...</small></li>
<li><a href='http://www.nasaspaceflight.com/2008/10/ula-delta-ii-cosmo-3-live/' rel='bookmark' title='Permanent Link: ULA Delta II launches with COSMO-3'>ULA Delta II launches with COSMO-3</a> <small>A United Launch Alliance (ULA) Delta II launch vehicle has...</small></li>
<li><a href='http://www.nasaspaceflight.com/2009/04/live-ula-atlas-v-launch-with-wgs-2/' rel='bookmark' title='Permanent Link: LIVE: ULA Atlas V launches WGS-2 for USAF'>LIVE: ULA Atlas V launches WGS-2 for USAF</a> <small>United Launch Alliance (ULA) has launched the WGS-2 satellite on...</small></li>
</ol>]]></description>
			<content:encoded><![CDATA[<p>The Delta Mariner &#8211; carrying hardware elements targeting two future launches &#8211; collided with the Eggner&#8217;s Ferry Bridge over Kentucky Lake on Thursday night. However, despite extensive damage to the bridge, no serious injuries were reported. ULA have noted that there will be no mission impact to the Advanced Extremely High Frequency (AEHF-2) and Radiation Belt Storm Probes (RBSP) missions.</p>
<p><span id="more-22924"></span><strong>Delta Mariner Accident:</strong></p>
<p>The Mariner &#8211; which is capable of carrying up to three common booster cores on the 2,100 mile journey from Alabama to Florida &#8211; was originally designed to carry Delta IV hardware from the production plant to the launch sites, while the Atlas hardware was delivered from its production facility in Denver to the launch sites by aircraft.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z218.jpg"><img class="alignleft size-full wp-image-22926" title="Z2" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z218.jpg" alt="" width="346" height="269" /></a>This process was reviewed in 2009, when the Atlas V production line was consolidated in Decatur, leading to ULA evaluations into common transportation options for both vehicles and the potential cost savings.</p>
<p>In mid-2011, Atlas hardware began sharing a ride on the Delta Mariner, <a href="http://www.nasaspaceflight.com/2011/07/nasa-juno-frr-completed-atlas-delta-share-ride-mariner/" target="_blank">completing a dual shipment, carrying both Atlas and Delta stages to Florida for future missions</a>.</p>
<p>The ship was carrying an Atlas first stage and a Centaur upper stage for the April mission to launch the Air Force&#8217;s Advanced Extremely High Frequency (AEHF-2) satellite.</p>
<p>Advanced Extremely High Frequency -2 (AEHF-2) is set to become part of a series of communications satellites operated by the United States Air Force Air Force Space Command. The spacecraft will be used to relay secure communications for the Armed Forces of the United States, the British Armed Forces, the Canadian Forces and the military of the Netherlands.</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?topic=27868.0">Accident Thread</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?topic=2341.0">65 Launch Vehicle Manuals (L2)</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div>
<p><a href="http://www.nasaspaceflight.com/2010/08/ula-atlas-v-launch-with-aehf-gps-satellte/" target="_blank">The system will eventually consist of four spacecraft in geostationary orbits, with one bird already in orbit</a>. AEHF is replacing the older Milstar system and will operate at 44 GHz Uplink (EHF band) and 20 GHz Downlink (SHF band).</p>
<p>The vessel was also shipping an interstage adapter for NASA&#8217;s Radiation Belt Storm Probes (RBSP) mission, scheduled to launch in August.</p>
<p>RBSP is being designed to help us understand the Sun&#8217;s influence on Earth and Near-Earth space by studying the Earth&#8217;s radiation belts on various scales of space and time.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z415.jpg"><img class="alignleft size-full wp-image-22929" title="Z4" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z415.jpg" alt="" width="350" height="238" /></a>The instruments on NASA&#8217;s Living With a Star Program&#8217;s (LWS) Radiation Belt Storm Probes (RBSP) mission will provide the measurements needed to characterize and quantify the plasma processes that produce very energetic ions and relativistic electrons.</p>
<p>The RBSP mission is part of the broader LWS program whose missions were conceived to explore fundamental processes that operate throughout the solar system and in particular those that generate hazardous space weather effects in the vicinity of Earth and phenomena that could impact solar system exploration.</p>
<p>RBSP instruments will measure the properties of charged particles that comprise the Earth&#8217;s radiation belts, the plasma waves that interact with them, the large-scale electric fields that transport them, and the particle-guiding magnetic field.</p>
<p>The two RBSP spacecraft will have nearly identical eccentric orbits. The orbits cover the entire radiation belt region and the two spacecraft lap each other several times over the course of the mission. The RBSP in situ measurements discriminate between spatial and temporal effects, and compare the effects of various proposed mechanisms for charged particle acceleration and loss.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z511.jpg"><img class="alignleft size-full wp-image-22930" title="Z5" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z511.jpg" alt="" width="350" height="210" /></a>The Delta Mariner, owned and operated by Foss Marine, made contact with the Eggner Ferry Bridge at US Highway 68 and Kentucky Highway 80 over the Tennessee River Thursday evening at 8:15 pm. Central Time resulting in a portion of the bridge collapsing, noted ULA in a release.</p>
<p>Kentucky Transportation Cabinet (KYTC) spokesperson Keith Todd told the media that it was a miracle no one was killed, as there were four cars on the bridge and an off duty officer about to cross. Despite damaging two spans of the bridge, no vehicles were on those sections when the accident occurred.</p>
<p>While an investigation will likely reveal the cause of the accident, it appears the ship may have been off course, or mis-directed, given the bridge has lights that span navigable waterways.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z317.jpg"><img class="alignleft size-full wp-image-22927" title="Z3" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z317.jpg" alt="" width="350" height="210" /></a>One of the spans of the bridge was completely destroyed and became wrapped around the around the front portion of the vessel, but appears to have avoided any hull damage. 20 crewmembers were on board the Delta Mariner, none of which were injured during the accident.</p>
<p>&#8220;The Mariner cargo area of the ship and the flight hardware did not experience any damage. The hardware is well instrumented and all data from these instruments is being reviewed to confirm that there were no issues. The Coast Guard is conducting an investigation,&#8221; added the ULA statement.</p>
<p>(Images: ULA, Associated Press and KYTC).</p>
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		<title>Opportunity&#8217;s eight years on Mars: A story of science and endurance</title>
		<link>http://www.nasaspaceflight.com/2012/01/opportunitys-eight-years-mars-story-science-endurance/</link>
		<comments>http://www.nasaspaceflight.com/2012/01/opportunitys-eight-years-mars-story-science-endurance/#comments</comments>
		<pubDate>Wed, 25 Jan 2012 05:05:51 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
				<category><![CDATA[Featured]]></category>
		<category><![CDATA[Other]]></category>
		<category><![CDATA[Unmanned]]></category>
		<category><![CDATA[Mars]]></category>
		<category><![CDATA[MER]]></category>
		<category><![CDATA[Opportunity Rover]]></category>

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		<description><![CDATA[Eight years ago today (January 25, 2004), the Mars Exploration Rover -B (MER -B) slammed into the Martian atmosphere and executed a successful Entry, Descent, and Landing on the Red Planet &#8211; beginning what was supposed to be 90 days of science operations on the surface of Mars. Eight years and 2,922 Earth-days later, Opportunity [...]


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			<content:encoded><![CDATA[<p>Eight years ago today (January 25, 2004), the Mars Exploration Rover -B (MER -B) slammed into the Martian atmosphere and executed a successful Entry, Descent, and Landing on the Red Planet &#8211; beginning what was supposed to be 90 days of science operations on the surface of Mars. Eight years and 2,922 Earth-days later, Opportunity continues its mission of exploration of the Martian surface, unlocking the mysteries of Mars and serving as a symbol of endurance while paving the way for future human missions to the Red Planet.</p>
<p><span id="more-22855"></span><strong>Gearing up for an ambitious mission on Mars:</strong><br />
 <br />
Like its twin rover, Spirit, Opportunity&#8217;s mission was based on 90-solar day mission on surface of Mars. A solar day is based on planetary Mars timekeeping based on Mars&#8217; orbital rotation rate.<br />
 <br />
A solar day on Mars is clocked at 24 hours 39 minutes 35.24409 seconds. Compared to Earth&#8217;s 24 hour 00 minute 00.002 second solar day length, the difference in the Earth-Mars solar day results in the Martian solar day lasting 2.7% longer than Earth&#8217;s with a conversation factor of 1.027491 days to sols.<br />
 <br />
Thus, since landing on Mars, Opportunity has operated for 2,844 sols, equivalent to 2,922 standard Earth days (Earth sols).</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?board=49.0">Unmanned Forum Section</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=34.0">L2 Historical Section</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div>
<p>In turn, this long-duration mission puts Opportunity 2,754 sols over its predicted and planned 90 sol-day mission &#8211; meaning that Opportunity has functioned 30.6 times longer than anticipated as the rover and its mission control team celebrates its 8th Earth-year anniversary on Mars.</p>
<p>Over these 8 Earth-years on Mars, Opportunity has searched for scientific knowledge based on its original mission objectives, including the search for and characteristic of rocks and soils.</p>
<p>Other objectives of Opportunity&#8217;s ongoing mission include the determination of the distribution and composition of minerals, rocks, and soils surrounding the landing site (and beyond, at this point); determination of what geologic processes have shaped the local terrain and influenced the chemistry, including water or wind erosion, sedimentation, hydrothermal mechanisms, volcanism, and cratering; and the performance calibration and validation of surface observations of Mars made by the Mars Reconnaissance Orbiter to help determine the accuracy and effectiveness of various instruments that survey the Martian geology from orbit.</p>
<p>Moreover, Opportunity&#8217;s objectives have and continue to revolve around the search for iron-containing minerals, including the identification and quantification of the relative amounts of specific mineral types that contain water or were formed in water; the characterization of the mineralogy and textures of rocks and soils to determine the processes that created them; the search for geological clues to the environmental conditions that existed when liquid water was present; and the assessment of whether the past Martian environment was conducive for life.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z214.jpg"><img class="alignleft size-full wp-image-22857" title="Z2" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z214.jpg" alt="" width="348" height="348" /></a>To accomplish the tasks given to it, Opportunity was truly built to last. At a height of 4.9 ft, a width of 7.5 ft, and a length of 5.2 ft, the six-wheeled utility craft was constructed to power itself via solar panels installed on its &#8220;back.&#8221;</p>
<p>These solar panels, at peak operating condition (clear of Martian dust and dirt), were designed to produce 140 watts of power for four hours per day. The energy produced from the solar panels is then transferred to the Opportunity&#8217;s lithium ion batteries for storage and distribution &#8211; thus allowing the rover to conserve power when not needed and use energy during non-sunlit portions of the day.</p>
<p>Weighing in a 400 lbs, the craft was built with mobility in mind, needing to not only drive itself to specific locations determined by its control team, but also to navigate around obstacles while driving toward specific targets of interest.</p>
<p>Thus, each wheel on Opportunity was given its own motor as well as steering at the front and rear drive sections.</p>
<p>With a maximum speed of 2 in/s (with an average speed about one-fifth of this), Opportunity was also built with the ability to navigate grades on the Martian surface of up to 30 degrees.</p>
<p>Opportunity was also affixed with nine scientific experiments, including a panoramic camera to examine the texture, color, mineralogy, and structure of the local Martian terrain; a navigation camera for driving purposes; the Miniature Thermal Emission Spectrometer to identify &#8220;promising rocks and soil&#8221; for examination; and two Hazcams with 120 degree views for &#8220;additional data about its surroundings.&#8221;</p>
<p>Opportunity&#8217;s robotic arm was fixed with the Mossbauer spectrometer for close-up investigations of the mineralogy of iron-bearing rocks and soils; the Alpha particle X-ray spectrometer for close-up analysis of the abundances of elements that make up rocks and soils; magnets for collects magnetic dust particles; a Microscopic Imager for close-up, high-resolution images of rocks and soils; and the Rock Abrasion Tool (RAT) to expose fresh rock material for examination by instruments on-board the rover.</p>
<p><strong>Getting to Mars:</strong></p>
<p>Like the Space Shuttle orbiter Endeavour and the Mars rover Sojourner before it, the Mars Rover &#8216;Opportunity&#8217; was named through a student essay competition. The winning entry was written by a Russian-American student who spoke of the spirit and opportunity to achieve her dreams in the United States after living a portion of her life in an orphanage.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z315.jpg"><img class="alignleft size-full wp-image-22858" title="Z3" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z315.jpg" alt="" width="347" height="256" /></a>With its construction and ground test/validation complete, Opportunity was transported to Florida where the rover underwent final testing and preparations for its trip to Mars.</p>
<p>With final preparations complete, Opportunity was folded up inside its aeroshell. Following the launch of Opportunity&#8217;s twin rover Spirit on 10 June 2003, Opportunity was transported to Launch Complex 17B at the Cape Canaveral Air Force Station, where the assembly was hoisted up and placed atop a Delta II Heavy rocket in mid-June for a June 28th launch.</p>
<p>Bad weather, an insulation problem, and a battery issue on the Delta II rocket forced a nine day delay to Opportunity&#8217;s launch.</p>
<p>On 7 July 2003, Opportunity&#8217;s launch team targeted the first of two instantaneous launch windows for the day. With just seconds to go in the countdown, an automatic cutoff was ordered by the launch computers when a fill-and-drain value on the Delta II indicated a sluggish response.</p>
<p>The launch team backed out of the terminal count and reconfigured for the second of only two instantaneous launch windows of the evening.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z413.jpg"><img class="alignleft size-full wp-image-22859" title="Z4" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z413.jpg" alt="" width="350" height="259" /></a>With the fill-and-drain valve issue fixed, the &#8220;go&#8221; was given to proceed with the count, and the Delta II Heavy rocket lifted off at 23:18:15 EDT with the Opportunity rover.</p>
<p>The launch was the first flight of the Delta II Heavy rocket configuration and occurred six days before the close of the Earth-Mars planetary alignment launch window.</p>
<p>After a 6.5 month cruise to Mars, Opportunity hit the Martian atmosphere just before midnight Eastern Standard Time on 24 January 2004.</p>
<p>Confirmation of a successful landing on Mars was received at 00:05 EST (05:05 UTC) 25 January 2004.</p>
<p><strong>A Hole-in-One landing and the first 90 sols on Mars:</strong></p>
<p>After descending through the Martian atmosphere, Opportunity&#8217;s encasement was engulfed in airbags to cushion the rover for the drop down and bounce/roll onto the Martian surface.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z59.jpg"><img class="alignleft size-full wp-image-22860" title="Z5" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z59.jpg" alt="" width="348" height="243" /></a>Landing on the Meridiani Plamun 25km downrange of its targeted landed sight, Opportunity&#8217;s airbag enclosed capsule rolled into an impact crater on the Martian surface before coming to a complete stop.</p>
<p>Upon opening of Opportunity&#8217;s encasement, the rover&#8217;s control team was amazed to find the rover sitting in the bottom of an impact crater and quickly described the landing as an inter-planetary &#8220;hole in one&#8221; &#8211; even though the rover was not targeting that specific area for landing.</p>
<p>After landing, Opportunity&#8217;s landing team christened the crater &#8220;Eagle crater,&#8221; and, in following with twin rover Spirit&#8217;s landing site, officially named Opportunity&#8217;s landing site &#8220;Challenger Memorial Station&#8221; in honor of the Space Shuttle Challenger and her crew who were lost in the Challenger/STS-51L launch accident &#8211; the 18th anniversary of which was just 3 days after Opportunity&#8217;s landing.</p>
<p>Upon examination of the landing crater, Opportunity showed that the crater was the darkest landing site ever visited by a spacecraft on Mars.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z76.jpg"><img class="alignleft size-full wp-image-22861" title="Z7" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z76.jpg" alt="" width="349" height="254" /></a>However, the landing presented a challenge for Opportunity&#8217;s control team as the rover would now have to climb a relatively steep embankment to get out of the crater.</p>
<p>From a stationary position on its landing bed, Opportunity observed a rock outcropping along the rim of the crater and a compilation of course gray grains in the otherwise reddish sand within the crater.</p>
<p>During this stationary checkout time, Opportunity&#8217;s control team discovered a problem with the rover&#8217;s robotic arm in the Joint 1 heater &#8211; specifically, that the heather on the joint that controls the side-to-side motion of the arm was stuck &#8220;on.&#8221;</p>
<p>An investigation revealed that the heater most likely failed during final assembly, test, and launch operations.</p>
<p>Since the rover was built with a safety device for this possibility, the T-stat box on the rover terminated the heater at a specific temperature and reactivated the heater once the joint&#8217;s temperature fell below a certain degree point.</p>
<p>This meant that Opportunity&#8217;s Joint 1 heater turned all for the duration of the Martian night and turned off for significant portions of the Martian day &#8211; a not ideal but &#8220;livable&#8221; issue.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z66.jpg"><img class="alignleft size-full wp-image-22862" title="Z6" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z66.jpg" alt="" width="349" height="244" /></a>By Sol 15, Opportunity was mobile and examining the rock outcroppings at Eagle crater. Observations made by Opportunity at the time led to the hypothesis that the rocks were formed from &#8220;fine grain or dust&#8221; instead of compacted sand as Earth sandstone is.</p>
<p>This hypothesis in turn led to the belief that the rocks were formed from volcanic flow, wind, or water. With water as a potential forming agent for the Eagle crater rock outcroppings, Opportunity&#8217;s goal of determining the potential that water had once existed on the surface of Mars for a long enough period to effect local geology was underway.</p>
<p>While Opportunity&#8217;s exploration at Eagle crater continued, the rover used its robotic arm RAT for the first time on Sol 30. Examination of the cut rock, located at the El Capitan outcropping, indicated signs of erosion (small, elongated voids in the rock visible both on the surface of the rock and in its interior after Opportunity&#8217;s drilling) that suggested the presence of liquid water at one point in Mars&#8217; past.</p>
<p>Specifically, scientists revealed that the voids were similar and &#8220;consistent&#8221; with vugs on Earth rocks.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z85.jpg"><img class="alignleft size-full wp-image-22863" title="Z8" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z85.jpg" alt="" width="348" height="273" /></a>Furthermore, Opportunity found evidence of water from the MIMOS II spectrometer. This instrument found evidence of the mineral jarosite, a mineral that contains hydroxide ions.</p>
<p>Opportunity&#8217;s crew also took this time to dig the first-ever trench by the Mars Rover pair by using the Opportunity&#8217;s front wheels. The process, which took less than an half-hour, created a trench 20 inches long by 4 inches deep.</p>
<p>The resultant dig revealed a &#8220;clotty texture&#8221; to the soil in the upper part of the trench and bright soil in the trench&#8217;s bottom.</p>
<p>The dig also revealed rounded, shiny pebbles and fine-grained soil particles too small for the rover&#8217;s microscope to discern.</p>
<p><strong>Beyond the 90-sol-day warranty - Opportunity at Endurance Crater:</strong></p>
<p>After leaving its landing site behind, Opportunity reached Endurance crater on Sol 95 &#8211; five days beyond its expected life time on Mars.</p>
<p>After completing a circumnavigation of the crater, Opportunity was directed toward the rock Lion Stone, which it arrived at 12 days after making it to Endurance crater.</p>
<p>Opportunity&#8217;s investigations of this rock found that it had a similar composition as those found at Eagle Crater.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z93.jpg"><img class="alignleft size-full wp-image-22865" title="Z9" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z93.jpg" alt="" width="349" height="219" /></a>By 4 June 2004, Opportunity&#8217;s team made the decision to send the rover itself into Endurance crater to examine an interesting area of rocks. This decision was made with the knowledge that the rover may not have been able to climb back out of the crater.</p>
<p>Opportunity began its descent into Endurance crater on 8 June 2004 before immediately backing out of the crater to test its descent angle. The information provided by this drive in/drive out maneuver confirmed that the angle of the crater&#8217;s surface was well within Opportunity&#8217;s operating limits.</p>
<p>After driving into Endurance crater on 12 June 2004, Opportunity spent 180 sols inside the crater examining the various rock formations &#8211; and even observing Earth-like wispy clouds in Mars&#8217; atmosphere.</p>
<p>During this time, Opportunity returned valuable scientific data on the soil composition and sedimentary geology of Endurance crater.</p>
<p><strong>A Stellar Find for Opportunity and a drive south:</strong></p>
<p>After completing operations at Endurance crater, Opportunity&#8217;s team commanded the rover to begin driving toward its own discarded heat shield that protected it during Martian atmospheric entry almost one year prior.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z102.jpg"><img class="alignleft size-full wp-image-22866" title="Z10" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z102.jpg" alt="" width="348" height="233" /></a>While conducting this examination of its heat shield, Opportunity stumbled upon a rock that would prove to be one the rover&#8217;s most significant finds: a meteorite on the surface of Mars.</p>
<p>Discovered on Sol 345, the meteorite was the first one ever discovered on a planet other than Earth (though two meteorites had already been discovered on the Moon), and was first identified an &#8220;unusual&#8221; because it had an infrared spectrum similar in appearance to a reflection of the sky of Mars.</p>
<p>Measurements and examinations by Opportunity showed the meteorite was composed of 93 percent iron and 7 percent nickel.</p>
<p>Because of a lack of knowledge of Mars&#8217; environment, whether the meteorite fell to Mars relative recently or several millions if not billions of years ago is unknown.</p>
<p>Opportunity has since found, to date, five similar meteorites.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z119.jpg"><img class="alignleft size-full wp-image-22867" title="Z11" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z119.jpg" alt="" width="347" height="243" /></a>After this discovery, Opportunity&#8217;s team directed the rover to dig another trench before setting off for Vostok crater.</p>
<p>After reaching Vostok crater and spending a few days in the vicinity, Opportunity was commanded southward to the &#8220;etched terrain.&#8221;</p>
<p>During this time, Opportunity set a single-day distance driving record by travelling 772 ft.</p>
<p>Stopping for six days to investigate soil surface ripples on the Meridiani Planum, Opportunity became the unwitting victim in a sand trap approximately 20 Martian days after leaving the rippled sands.</p>
<p>Opportunity became stuck in the sand on 26 April 2005 after attempting to climb over a dune that measured only 12 inches (30 centimeters) in height.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z122.jpg"><img class="alignleft size-full wp-image-22868" title="Z12" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z122.jpg" alt="" width="351" height="244" /></a>The dune was quickly dubbed &#8220;purgatory dune&#8221; because of the predicament it now posed.</p>
<p>Spending an agonizing 38 Sols stuck in the sand, Opportunity was eventually able to free itself after ground controllers simulated the condition here on the Earth.</p>
<p>Through a precise series of commands and maneuvers, Opportunity painstakingly moved only centimeters at a time so mission controllers could monitor progress and assess a best next move scenario after each labored movement forward.</p>
<p>After being freed, Opportunity spent 12 Sols studying purgatory dune before continue southward toward its target of Erebus crater.</p>
<p><strong>The road to Victoria crater:</strong></p>
<p>While Erebus crater was, in-hindsight (considering Opportunity&#8217;s longevity), always a stop-over on the way to Victoria crater, the year-long period between Opportunity&#8217;s arrival at Erebus (October 2005) and arrival at Victoria (September 2006) crater was a year filled with notable milestones for the mission, including the first dust storm endured by the rover, a cleaning event on its solar panels, and further problems with the rover&#8217;s robotic scientific arm.</p>
<p>During this time, a new program was uploaded to Opportunity that would prevent the rover from becoming stuck in another sand dune.</p>
<p>This program proved invaluable on Sol 603 when the program triggered an &#8220;all stop&#8221; command to Opportunity when the rover&#8217;s wheel-slip percentage reached 44.5 percent &#8211; thus preventing Opportunity from getting stuck in another sand dune.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z133.jpg"><img class="alignleft size-full wp-image-22869" title="Z13" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z133.jpg" alt="" width="348" height="230" /></a>By Sol 628, though, the rover was engulfed in a dust storm that lasted three days. The storm deposited numerous quantities of dust onto the rover&#8217;s solar panels and reduced total power generation on the rover.</p>
<p>However, as luck would have it, a sudden cleaning event took place less than three weeks after the dust storm, restoring Opportunity&#8217;s power generating capabilities to 80 percent of maximum.</p>
<p>The cleaning events occur when Martian winds blew the dust off the solar panels.</p>
<p>But by this point, Opportunity&#8217;s control team was battling a further issue with the rover&#8217;s Joint 1 heater.</p>
<p>As Opportunity approached its first Martian winter back in May 2004, the control team commanded the rover into deep sleep at night, a procedure which disconnected Opportunity&#8217;s systems from the main battery &#8211; thus preventing the Joint 1 heater from remaining &#8220;on&#8221; throughout the day and night as temperatures dropped in the Martian winter.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z142.jpg"><img class="alignleft size-full wp-image-22870" title="Z14" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z142.jpg" alt="" width="349" height="253" /></a>However, this procedure exposed the mechanical joint to extreme temperature swings during the day and night and eventually led to the stall of the Joint 1 motor on 25 November 2005.</p>
<p>At this point, Opportunity&#8217;s control team commanded the rover to send a higher-than-normal electrical current the arm to unstow it. This approach worked, though the joint would occasionally stall.</p>
<p>By late March 2006, after 760 sols on Mars, Opportunity departed Erebus crater for Victoria crater, arriving 191 sols later.</p>
<p><strong>Time at Victoria crater &#8211; A struggle for survival:</strong></p>
<p>Upon arriving at Victoria carter on 16 September 2006, Opportunity photographed the crater and returned the first substantial views of Victoria&#8217;s 7 kilometer wide impact crater.</p>
<p>During initial observations at Victoria, Opportunity revealed a dune field at the bottom of the crater as well as a slope leading into the crater itself.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z152.jpg"><img class="alignleft size-full wp-image-22872" title="Z15" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z152.jpg" alt="" width="350" height="243" /></a>While Opportunity investigated the rim of Victoria crater, mission controllers sent a software upgrade package to the rover that allowed it to make internal decisions on whether or not to transmit images back to Earth and whether or not to extend its robotic arm for scientific investigation.</p>
<p>By mid-May 2007, while crater rim observations and investigations continued, a series of significant cleaning events allowed for unprecedented power increases to the rover to levels not seen since Sol 18 of the mission.</p>
<p>This dramatic increase in power generating capability came at the best time possible as residual daily power was stored in Opportunity&#8217;s batteries just a month before devastating dust storms nearly claimed the rover.</p>
<p>Beginning in June 2007, Mars&#8217; six Earth-year dust storm cycle began, clouding the Martian atmosphere in dust and blocking 99 percent of sunlight from reaching Opportunity&#8217;s solar panels &#8211; while at the same covering the rover&#8217;s solar panels and significantly reducing the rover&#8217;s ability to gather the small amount of sunlight actually reaching it.</p>
<p>As power level dropped to dangerously low levels, NASA released a statement saying, &#8220;We&#8217;re rooting for our rovers to survive these storms, but they were never designed for conditions this intense.&#8221;</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z161.jpg"><img class="alignleft size-full wp-image-22873" title="Z16" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z161.jpg" alt="" width="350" height="276" /></a>Normal solar panel generation of 700 watt-hours energy per day dropped to only 128 watt-hours on 18 July 2007 on Opportunity. As a result, Opportunity began draining its batteries to preserve system power and heating requirements.</p>
<p>The rover&#8217;s control team, in response, commanded the rover to only communicate with Earth every three days to converse power for its heaters.</p>
<p>By late-July 2007, Opportunity was barely getting enough solar energy each day to survive, and the temperature in the rover&#8217;s electronics module was dropping. At this point, NASA stated that if temperatures continued to drop, Opportunity&#8217;s low-power fault program could trip, disabling the rover&#8217;s batteries and putting Opportunity into sleep mode.</p>
<p>&#8220;There is a real risk that Opportunity will trip a low-power fault. When a low-power fault is tripped, the rover&#8217;s systems take the batteries off-line, putting the rover to sleep and then checking each sol to see if there is sufficient available energy to wake up and perform daily fault communications.</p>
<p>&#8220;If there is not sufficient energy, Opportunity will stay asleep. Depending on the weather conditions, Opportunity could stay asleep for days, weeks or even months, all the while trying to charge its batteries with whatever available sunlight there might be.&#8221;</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z171.jpg"><img class="alignleft size-full wp-image-22874" title="Z17" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z171.jpg" alt="" width="349" height="230" /></a>At this point, NASA also stated that there was a real chance that Opportunity, if placed into sleep mode, would never wake up.</p>
<p>But despite these abysmal odds, Opportunity never tripped its low-power fault, and by 7 August 2007, with the dust storms beginning to subside, power levels were sufficient for Opportunity to start taking pictures of the Martian dust storm again.</p>
<p>By 21 August, Opportunity&#8217;s batteries were fully charged, and the rover began driving again for the first time since the dust storm began &#8211; an amazing endurance story for the rover that had, by this point, survived the &#8220;un-survivable&#8221; scenario on Mars&#8217; surface during full-fledged operations three years beyond its expected 90 sol day death date from low power levels because of predicted dust accumulation on its solar panels.</p>
<p>Recovering from the dust storm, Opportunity began its descent into Victoria crater on 11 September 2007 to test the terrain&#8217;s stability and slope gradient.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z181.jpg"><img class="alignleft size-full wp-image-22875" title="Z18" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z181.jpg" alt="" width="349" height="247" /></a>With final checks complete, Opportunity descended the Duck Bay ramp into Victoria crater on 13 September 2007 where it explored, for the next Earth-year, the rock composition of Duck Bay and the face of Cape Verde in great scientific detail.</p>
<p>By 15 April 2008, while still inside Victoria crater, Opportunity&#8217;s robotic arm once again failed to respond to commands, and the Joint 1 motor stalled at the beginning of unstowing operations.</p>
<p>The motor stalled on all follow-up unstow attempts &#8211; something the differed from previous unstow stalls where the motor worked on subsequent attempts.</p>
<p>A month of testing followed, during which controllers monitored resistance on the joint at various times in the day.</p>
<p>After rover wake up on Sol 1531 (14 May 2008), Opportunity was commanded to unstow its robotic arm. The command worked, and the arm extended from underneath the rover.</p>
<p>At this point, the decision was made to never stow the arm again, and a safe, arm-extended drive configuration was determined and implemented.</p>
<p>Thus, since May 2008, nearly 4 years ago and for half its time on Mars, Opportunity has driven across the surface of Mars with its robot arm fully extended out in front of it.</p>
<p><strong>A new mission target - Endeavour crater:</strong></p>
<p>With the rover in good health, Opportunity&#8217;s control team elected to send the rover on a 14 mile (22 kilometer) trek to Endeavour crater.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z191.jpg"><img class="alignleft size-full wp-image-22876" title="Z19" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z191.jpg" alt="" width="350" height="278" /></a>Emerging from Victoria crater between 24-28 August 2008 (Sols 1630-1634), Opportunity began the impressive trek for Endeavour crater, stopping along the way to investigate various &#8220;dark cobbles&#8221; on the Meridiani Planum.</p>
<p>Endeavour crater was chosen in large part due to expectations that deeper stacks of rocks would be seen at Endeavour crater than at Victoria crater. Furthermore, the team opted to send Opportunity to Endeavour crater following the discovery of phyllosilicate, clay-bearing rock at Endeavour crater &#8211; rock that is hospitable to life.</p>
<p>During the predicted two year drive to Endeavour crater, Opportunity was temporarily out of contact with Earth during the Solar conjunction of November/December 2008 at which time Earth and Mars were on opposite sides of the sun from one another.</p>
<p>By March 2009, Opportunity&#8217;s cameras could see the rim of Endeavour crater, as well as Iazu crater &#8211; which was 38 kilometers (24 miles) away from the rover at the time.</p>
<p>By 18 July 2009 (Sol 1850), Opportunity was directed to reverse course away from Endeavour crater and toward a large, black rock.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z20.jpg"><img class="alignleft size-full wp-image-22877" title="Z20" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z20.jpg" alt="" width="349" height="307" /></a>The rover reached the rock ten Earth-days later, at which point it was discovered that the rock was yet another meteorite.</p>
<p>After examination of the rock, Opportunity was again commanded to drive toward Endeavour crater, but was stopped again on Sol 2022 when it found yet another meteorite. After examining this meteorite for 12 Sols, Opportunity found yet another meteorite on Sol 2038.</p>
<p>This time, the rover did a &#8220;drive by&#8221; investigation, taking photographs of the meteorite while continuing on toward Endeavour crater.</p>
<p>Opportunity again stopped on Sol 2061 (10 November 2009) to investigate a rock target that&#8217;s identity was not initially clear.</p>
<p>It was eventually determined that the rock was rock ejecta material from deep within Mars.</p>
<p>Investigation of the rock ejecta concluded on Sol 2122 (12 January 2010), and the rover arrived at Concepcion crater on 28 January 2010.</p>
<p>After circumnavigating the crater, Opportunity once again set out for Endeavour crater.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z215.jpg"><img class="alignleft size-full wp-image-22878" title="Z21" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z215.jpg" alt="" width="349" height="273" /></a>By 5 May 2010, a new route to Endeavour crater was plotted to avoid potentially hazardous sand dunes.</p>
<p>Then, on Sol 2246 (19 May 2010), the Opportunity rover, despite arriving on Mars after its twin rover Spirit, became the longest-surviving surface mission on Mars, surpassing the previous 2245 Sol duration set by the Viking 1 mission from the late 1970s to early 1980s.</p>
<p>On Sol 2420 (14 November 2010), Opportunity&#8217;s odometer passed the 25 kilometer mark &#8211; shattering all estimates for how far the rover would actually drive on the surface of Mars.</p>
<p>In mid-December 2010, Opportunity began several weeks of observations at Santa Maria crater &#8211; observations that were compared to orbital data from the Mars Reconnaissance Orbiter (MRO).</p>
<p>At the conclusion of the 2010 Earth-year, Opportunity had driven more miles since leaving Victoria crater in August 2008 (the equivalent of 1 Martian year) than it had in any previous year &#8211; all while being 4-6 years beyond its originally estimated life span.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z221.jpg"><img class="alignleft size-full wp-image-22879" title="Z22" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z221.jpg" alt="" width="348" height="242" /></a>Opportunity spent the two-week solar conjunction of early 2011 at Santa Maria crater before beginning the final 6.5 kilometer journey to Endeavour crater in late March 2011.</p>
<p>By 1 June 2011, Opportunity passed the 30km life-time traverse mark &#8211; a distance 50 times greater than its operational designed traverse distance.</p>
<p>By 17 June 2011, Opportunity had driven 20 miles on the surface of Mars.</p>
<p>After 3 years of travels, Opportunity safely and successfully arrived at Endeavour crater on 9 August 2011 after traveling 13 miles from Victoria crater &#8211; a distance more than half of its total traversed distance on Mars.</p>
<p>The rover&#8217;s arrival point at Endeavour crater was quickly named &#8220;Spirit Point&#8221; by Opportunity&#8217;s control team in honor of Opportunity&#8217;s twin, Spirit, which did not survive the 2010 Martian winter.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z231.jpg"><img class="alignleft size-full wp-image-22880" title="Z23" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z231.jpg" alt="" width="351" height="244" /></a>Upon arriving at the crater, Opportunity quickly confirmed that the rocks on the rim of crater were older than any other rock previously studied by the rover, and quickly discovered Martian phenomenon not previously seen.</p>
<p>And then, in early December 2011, Opportunity made what is, at this time, its most important discovery while analyzing the &#8220;Homestake&#8221; formation.</p>
<p>Instruments on the rover were able to confirm that the &#8220;Homestake&#8221; formation is composed of gypsum &#8211; a mineral that does not occur except in the presence of water.</p>
<p>The rock was quickly nick-named &#8220;slam dunk&#8221; as it finally provided hard evidence that liquid water once flowed on Mars &#8211; thus providing substantial support for one of Opportunity&#8217;s primary mission scientific objectives.</p>
<p><strong>An enduring legacy:</strong></p>
<p>Throughout its eight year tenure on Mars, the rover Opportunity has greatly and in many ways drastically increased our knowledge of Mars as well as how our technology survives on the Martian surface.</p>
<p>Based on its tremendous scientific finds, life-span, and endurance beyond all odds, several honors have been conferred upon the Opportunity rover. Asteroid 39382 was officially named Opportunity in honor of the rover.</p>
<p>Furthermore, Opportunity is one of only 13 robots to be inducted into the robot hall of fame alongside the da Vinci Surgical System, fellow Mars rover Sojourner, Unimate (the first industrial robot which worked on the General Motors assembly line in 1961), and twin rover Spirit.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z241.jpg"><img class="alignleft size-full wp-image-22881" title="Z24" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z241.jpg" alt="" width="350" height="270" /></a>Moreover, while Opportunity&#8217;s landing site paid tribute to the Space Shuttle Challenger and her crew, Opportunity itself stands as a tribute and memorial to the men and women lost in the September 11th terrorist attacks on the World Trade Center, as metal from the twin towers was repurposed and used as cable protection shields on the twin rovers Opportunity and Spirit.</p>
<p>But perhaps the best way to continue to remember Opportunity, even though its time on Mars is not yet over, is the tremendous distance and longevity of the rover.</p>
<p>Travelling 21.33 miles, Opportunity has exceeded by more the 50 times the driving distance it was built for, it survived a severe Martian dust storm despite legitimate fears that it would not, it has conducted long-term investigations of four craters and entered, under its own power, two craters (not including the hole-in-one landing in Eagle Crater), and it has survived 30.6 times longer than originally planned.</p>
<p>(All Images via NASA, NASA JPL, NASA APOD).</p>
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		<title>ULA Delta IV successfully launches the fourth WGS spacecraft</title>
		<link>http://www.nasaspaceflight.com/2012/01/live-ula-launch-delta-iv-fourth-wgs/</link>
		<comments>http://www.nasaspaceflight.com/2012/01/live-ula-launch-delta-iv-fourth-wgs/#comments</comments>
		<pubDate>Thu, 19 Jan 2012 23:06:23 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
				<category><![CDATA[Featured]]></category>
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		<description><![CDATA[United Launch Alliance have conducted the United States&#8217; first orbital launch of the year on Thursday, when their Delta IV launched with the fourth Wideband Global Satcom spacecraft. Liftoff from SLC-37B at the Cape Canaveral Air Force Station was on schedule for the beginning of a 93-minute launch window which opened at 19:38 local time [...]


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<li><a href='http://www.nasaspaceflight.com/2009/03/live-delta-ii-launch-penultimate-gps-iir-satellite-2/' rel='bookmark' title='Permanent Link: Delta II launches penultimate GPS-IIR satellite'>Delta II launches penultimate GPS-IIR satellite</a> <small>A United Launch Alliance (ULA) Delta II rocket has launched this...</small></li>
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			<content:encoded><![CDATA[<p>United Launch Alliance have conducted the United States&#8217; first orbital launch of the year on Thursday, when their Delta IV launched with the fourth Wideband Global Satcom spacecraft. Liftoff from SLC-37B at the Cape Canaveral Air Force Station was on schedule for the beginning of a 93-minute launch window which opened at 19:38 local time (00:38 on Friday in UTC).</p>
<p><span id="more-22780"></span><strong>Delta IV/WGS:</strong></p>
<p>Wideband Global Satcom, or WGS, is one of three next-generation communications systems being introduced by the US military, along with the Advanced Extremely High Frequency (AEHF) and Mobile User Objective System (MUOS). Originally named Wideband Gapfiller Satellite, WGS was originally conceived as a temporary replacement for the aging Milstar system, until AEHF became operational.</p>
<p>However, its primary mission has become supplementing and eventually replacing the Defense Satellite communications System, or DSCS. Having started as a US programme, WGS has grown to include several other countries, including Australia, New Zealand, Canada, Denmark, the Netherlands and Luxembourg.</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?topic=27051.0">Delta IV/WGS UPDATES</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?topic=2341.0">65 Launch Vehicle Manuals (L2)</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div>
<p>The WGS-4 satellite is first Block II WGS satellite, a modification on the original series which incorporates a new bypass system which triples the rate at which reconnaissance aircraft can relay images via the system.</p>
<p>Three Block I WGS satellites are already in orbit; <a href="http://www.nasaspaceflight.com/2007/10/atlas-v-launches-with-wgs-sv-1/" target="_blank">WGS-1 or USA-195 was launched by an Atlas V 421 in October 2007</a>, with <a href="http://www.nasaspaceflight.com/2009/04/live-ula-atlas-v-launch-with-wgs-2/" target="_blank">WGS-2, or USA-204, following in April 2009</a>, also on an Atlas. In December 2009, <a href="http://www.nasaspaceflight.com/2009/12/live-ula-delta-iv-launch-with-wgs-3/" target="_blank">WGS-3 or USA-211 was launched on the first flight of the Delta IV-M+(5,4).</a></p>
<p>Including those already on orbit, current plans call for nine WGS satellites to be launched, with a tenth expected to be ordered in the near future. Each satellite has a mass of 5,990 kilograms, and is capable of receiving and transmitting data on frequencies of 500 megahertz and 1 gigahertz, at rates of up to 3.6 gigabits per second. Each spacecraft can cover 19 areas simultaneously, with eight steerable x-band transponders and ten steerable ka-band transponders.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z210.jpg"><img class="alignleft size-full wp-image-22782" title="Rollout of Delta IV Medium WGS-4" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z210.jpg" alt="" width="300" height="321" /></a>Boeing is the prime contractor for WGS, with the satellites being based around its BSS-702 satellite bus. Each spacecraft is equipped with an R-4D apogee motor for orbit raising and circularisation manoeuvres, and four XIPS-25 ion engines which will be also be used for orbit circularisation, as well as stationkeeping in geosynchronous orbit.</p>
<p>The satellite will use a pair of solar arrays, equipped with gallium arsenide cells, to generate power. The satellite will be controlled by the US Air Force&#8217;s Third Space Operations Squadron, which is based at Schriever Air Force Base in Colorado.</p>
<p>The Delta IV used to launch WGS-4 is Delta 358. Unusually, the rocket&#8217;s flight or &#8220;Delta number&#8221;, has not been painted on the rocket &#8211; the number is usually present within a blue triangle on the interstage which symbolises the Delta series of rockets, however on Delta 358 this triangle has been left blank.</p>
<p>Delta 358 was a Delta IV Medium+(5,4) rocket, consisting of a Common Booster Core first stage, with four GEM-60 solid rocket motors, and a five metre Delta Cryogenic Second Stage.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z310.jpg"><img class="alignleft size-full wp-image-22783" title="Rollout of Delta IV Medium WGS-4" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z310.jpg" alt="" width="350" height="285" /></a>The largest of the Delta IV Medium+ configurations, the (5,4) has only flown once before; deploying the last WGS satellite in December 2009.</p>
<p>The Common Core Booster is a cryogenically-fuelled stage, powered by a single RS-68 engine, burning liquid hydrogen and liquid oxygen. The main engine will ignite five and a half seconds ahead of launch, followed by the solid rocket motors two hundredths of a second before the countdown reaches zero.</p>
<p>The solid rocket motors provide additional thrust during early ascent, with two also being equipped with moveable nozzles for thrust vectoring, contributing to the vehicle&#8217;s attitude control during the initial stages of the flight.</p>
<p>At T-0, Delta 358 lifted off from Space Launch Complex 37, and begin its ascent towards orbit. Seven seconds later, it began a manoeuvre to attain an azimuth of 100.97 degrees out over the Atlantic Ocean, and pitched over to attain its planned ascent trajectory. At around 36 seconds after launch, the rocket passed through the sound barrier, and 50.1 seconds into its flight it passed through max-Q, the area of maximum dynamic pressure.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z56.jpg"><img class="alignleft size-full wp-image-22784" title="Rollout of Delta IV Medium WGS-4" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z56.jpg" alt="" width="333" height="317" /></a>The GEM-60 motors burnt out in pairs at 93.1 and 93.3 seconds after launch, with the thrust-vectoring pair being last to burn out. The two motors with fixed nozzles separated from the first stage 100 seconds into the flight, with the others following 2.35 seconds later.</p>
<p>Three minutes and 27 seconds after launch, the payload fairing separated from around the satellite. The fairing protects the spacecraft during its ascent through the atmosphere, but is no longer needed in space where the particle density is far lower.</p>
<p>The Delta IV-M+(5,4) uses a payload fairing which is a little over eight metres long, and has a diameter of five metres. Just under forty seconds after the fairing separates, the RS-68 shut down, having completed the first stage burn. Eight seconds later, the first and second stages separated by means of sixteen pneumatic actuators.</p>
<p>The second stage, or DCSS, is fuelled by the same cryogenic propellants as the first stage. It is powered by an RL10B-2 engine, with an extendable nozzle. Following separation, the nozzle deployed, before the engine ignited 13 seconds after staging to begin the first of two burns.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z64.jpg"><img class="alignleft size-full wp-image-22785" title="Rollout of Delta IV Medium WGS-4" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z64.jpg" alt="" width="328" height="315" /></a>This first burn lasted 16 minutes and 15.9 seconds, placing the vehicle into an initial parking orbit for a brief coast phase. This coast lasted for just seven minutes and 44.6 seconds, before the RL10 ignited again for its second burn. After firing for another three minutes and 8.3 seconds, the RL10 again cut off, completing powered ascent.</p>
<p>Nine minutes and 6.2 seconds after the completion of the second burn, or 40 minutes and 42 seconds after launch, the WGS-4 satellite was separated from the DCSS. According to United Launch Alliance, the target orbit at spacecraft separation will be one with a perigee of 440 kilometres, an apogee of 66,870 kilometres, and an inclination of 24 degrees to the equator.</p>
<p>WGS-4 manoeuvred from this supersynchronous transfer orbit into its operational geosynchronous orbit. Three minutes after spacecraft separation, the DCSS began a collision avoidance manoeuvre, which lasted about three minutes and 48 seconds. About half an hour later the upper stage will be safed with propellant tank blowdown, and a hydrazine depletion manoeuvre.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z48.jpg"><img class="alignleft size-full wp-image-22786" title="Rollout of Delta IV Medium WGS-4" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z48.jpg" alt="" width="349" height="263" /></a>Delta IV launches from Cape Canaveral are conducted from Space Launch Complex 37B. Originally built in the 1960s as a backup launch complex for the Apollo programme, it was used to test hardware which would be used in the moon landings. The first launch from the complex was of SA-5, the first all-up test of the Saturn I, and the first orbital launch of a Saturn rocket, on 29 January 1964.</p>
<p>The original Launch Complex 37 consisted of two pads, but with a single mobile service tower (MST) which could be moved between the two pads. Pad A was never used, whilst pad B, the same pad used by the Delta IV, was used by six Saturn I rockets followed by two Saturn IBs.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z74.jpg"><img class="alignleft size-full wp-image-22787" title="Z7" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z74.jpg" alt="" width="296" height="299" /></a>The last launch from the complex came in January 1968, when a Saturn IB launched Apollo 5; the first test flight of the Lunar Module in Earth orbit. Following the launch of Apollo 5, LC-37 was mothballed along with Launch Complex 34 ahead of the Apollo Applications programme, which would have seen additional flights of the Apollo spacecraft to Low Earth orbit, which would have made use of the Saturn IB. Of all the Applications proposals, only one ever flew; Skylab.</p>
<p>With only three manned flights required to support this, it was decided that it would be cheaper to convert Launch Complex 39 to accommodate the Saturn IB than to reactivate either LC-34 or LC-37, and the complex was demolished in the 1970s.</p>
<p>In the late 1990s, the site of the former Saturn launch complex was selected for use by the Delta IV, and rebuilt to support it. The new complex was first used for the maiden flight of the Delta IV, which occurred in 2002. Delta 358 will be the fifteenth Delta IV to use the complex, and the twenty-first launch from it overall.</p>
<p>Delta IV launches are conducted by United Launch Alliance, a company formed to operate the Delta II, Delta IV and Atlas V rockets on behalf of the US Government, Lockheed Martin and Boeing. The launch of WGS-4 was the 57th launch to be conducted by ULA since it formed in December 2006. ULA is aiming to conduct eleven Delta IV and Atlas V launches in 2012.</p>
<p>The launch of WGS-4 was the first orbital launch to be conducted by the United States this year. Last year the USA conducted 18 launches, with 17 successful and one failure, however it was overtaken by China in terms of total launches for the first time. The next US orbital launch is currently scheduled for 16 February, when an Atlas V 551 will orbit the first MUOS communications satellite.</p>
<p>The next Delta IV launch is expected to occur in March, when the first Delta IV-M+(5,2) will launch from Vandenberg, carrying the NROL-25 mission for the US National Reconnaissance Office. The next WGS satellite is expected to launch in about a year&#8217;s time, also aboard a Delta IV.</p>
<p>(Images via ULA and NASA)</p>
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		<title>Enabling the future: NASA call for exploration revolution via NIAC concepts</title>
		<link>http://www.nasaspaceflight.com/2012/01/enabling-future-nasa-call-exploration-revolution-niac-concepts/</link>
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		<pubDate>Tue, 10 Jan 2012 01:40:14 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
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		<description><![CDATA[NASA&#8217;s Space Technology Program announced on Monday they are looking for what they describe as &#8220;far-out&#8221; concepts and ideas, as part of the Agency&#8217;s NASA Innovative Advanced Concepts (NIAC) program. Otherwise tagged as &#8220;game-changing&#8221;, such concepts range from advanced space suits to new propulsion methods for exploration spacecraft. NIAC: The original NIAC ran from 1998-2007, [...]


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			<content:encoded><![CDATA[<p>NASA&#8217;s Space Technology Program announced on Monday they are looking for what they describe as &#8220;far-out&#8221; concepts and ideas, as part of the Agency&#8217;s NASA Innovative Advanced Concepts (NIAC) program. Otherwise tagged as &#8220;game-changing&#8221;, such concepts range from advanced space suits to new propulsion methods for exploration spacecraft.</p>
<p><span id="more-22628"></span><strong>NIAC:</strong></p>
<p>The original NIAC ran from 1998-2007, &#8220;inspiring and nurturing revolutionary concepts that could transform future aerospace endeavors.&#8221; Returning in 2011, NIAC&#8217;s goal was to fund &#8220;early studies of visionary, long term concepts &#8211; aerospace architectures, systems, or missions (not focused technologies).&#8221;</p>
<p>This second call for proposals follows inaugural selection of Phase I concepts, which are now under study.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z9.jpg"><img class="alignleft size-full wp-image-22643" title="Z9" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z9.jpg" alt="" width="348" height="231" /></a>The 2011 effort resulted in funding for 30 distinct project advanced technology proposals which will better help the agency explore space. Each approach &#8211; which ranged from changing the course of orbital debris, a self stabilizing spacesuit using flywheels, the exciting technology of 3-D printing and numerous propulsion and power concepts for future missions &#8211; each received $100,000 for one year of studies.</p>
<p>Now, just days into 2012, NIAC are seeking proposals for revolutionary concepts with the potential to transform future aerospace missions. The proposed concepts should enable new capabilities or significantly alter current approaches to launching, building and operating space systems.</p>
<p>In announcing the new effort, NIAC noted that projects are chosen for their innovative and visionary characteristics, technical substance, and early development stage &#8211; ten years or more from use on a mission. NIAC&#8217;s current portfolio of diverse and innovative ideas represents multiple technology areas, including power, propulsion, structures and avionics.</p>
<p>&#8220;NIAC is a forward-looking program that captures what&#8217;s great about America&#8217;s space program,&#8221; said Michael Gazarik, director of NASA&#8217;s Space Technology Program. &#8220;NASA is looking for futuristic concepts that may enable leaps forward in how we work in and explore the space frontier.</p>
<p>&#8220;Equally important, we&#8217;re asking for ideas from all sources: American citizen-inventors or educators working out of their garage to the visionary small business owners fueling our nation&#8217;s economy.&#8221;</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?board=26.0">Advanced Forum Section</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=29.0">L2 Future Spacecraft</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=48.0">L2 BEO Launch Hardware</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div>
<p>Based on the large number of submissions received from 2011&#8242;s NIAC call for proposals, 2012&#8242;s Phase I solicitation will incorporate a two-step process &#8211; of which NASA expects to award funding for approximately 15 proposals.</p>
<p>&#8220;NIAC will accept short proposals, limited to two pages in length, until February 9. After review, NASA will invite those whose concepts are of interest to the agency to submit a full proposal of no more than ten pages. Full proposals will be due April 16,&#8221; the NASA release noted.</p>
<p>Those selected will receive up to $100,000 for one year to advance the innovative space technology concept and help NASA meet current operational and future mission requirements. Selection announcements are expected this summer.</p>
<p>The number of Phase I awards also will be balanced with NASA&#8217;s selection of Phase II awards. Phase II awards will be selected from Phase I concepts submitted last year that the agency decides to advance.</p>
<p>&#8220;NASA&#8217;s early investment and partnership with creative scientists, engineers and citizen inventors will pay huge technological dividends and help maintain America&#8217;s leadership in the global technology economy,&#8221; added the NASA release.</p>
<p>The solicitation is open to all United States citizens and researchers working in the United States, including NASA civil servants.</p>
<p><strong>Out-Of-The-Box Advances:</strong></p>
<p>While NIAC cover a large range of technologies, the need to move past the current chemical propulsion methods has been a long-standing wish for advancing the capability and execution of <a href="http://www.nasaspaceflight.com/?s=%28BEO%29" target="_blank">Beyond Earth Orbit (BEO) exploration</a>.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z53.jpg"><img class="alignleft size-full wp-image-22642" title="Z53" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z53.jpg" alt="" width="350" height="290" /></a>NASA administrator Charlie Bolden hinted at this wish via his announcement of the FY2011 budget proposal, in which he called for a study into a five year &#8220;game changing&#8221; propulsion study, as part of the changes proposed to the Heavy Lift Launch Vehicle (HLV) program, in tandem with the <a href="http://www.nasaspaceflight.com/2010/07/unemployed-ares-i-mobile-launcher-crawler-trip-august/" target="_blank">cancellation of the Constellation Program</a> (CxP).</p>
<p><a href="http://www.nasaspaceflight.com/2010/09/nasas-senate-bill-passes-dramatic-debate-vote-congress/" target="_blank">That proposal was changed via the 2010 Authorization Act</a>, which called for the <a href="http://www.nasaspaceflight.com/2011/06/managers-sls-announcement-after-sd-hlv-victory/" target="_blank">HLV to utilize hardware from the Space Shuttle Program (SSP) and Constellation Program</a> (CxP), as opposed to effectively mothballing <a href="http://www.nasaspaceflight.com/tag/hlv/" target="_blank">what is now the Space Launch System (SLS)</a> for at least five years.</p>
<p>NIAC appear to be looking towards the future from an &#8220;anyone got a better idea?&#8221; standpoint, calling for innovative propulsion and power concepts needed for future space mission operations. Such &#8220;out-of-the-box&#8221; thinking can be seen via the 2011 proposal presentations, which provide insight into the potential applications of future space exploration. (<a href="http://www.nasa.gov/offices/oct/early_stage_innovation/niac/" target="_blank">Link to presentations</a>).</p>
<p>Led by &#8220;The Potential for Ambient Plasma Wave Propulsion&#8221;, the 2011 resources provide introductions to some of the revolutionary ideas which could provide breakthroughs into advancing the exploration of deep space.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z33.jpg"><img class="alignleft size-full wp-image-22635" title="Z3" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z33.jpg" alt="" width="349" height="244" /></a>&#8220;Truly robust and affordable space exploration will require that we use all the available resources we can find in space,&#8221; noted James Gilland of the Ohio Aerospace Institute.</p>
<p>&#8220;Many planets, and the Sun, possess an ambient environment of magnetic fields and plasmas. Plasmas with magnetic fields can support a variety of waves, which transmit energy and or pressure, like light or sound waves. Many of these waves are at radio frequencies (kHz to MHz), and can be generated using the appropriate antenna.</p>
<p>&#8220;This concept simply uses an on‐board power supply and antenna on a vehicle that operates in the existing plasma. The spacecraft&#8217;s beams plasma waves in one direction with the antenna, to generate momentum that could propel the vehicle in the other direction, without using any propellant on the space ship. Such a system could maneuver in the plasma environment for as long as its power supply lasts, without refueling.</p>
<p>&#8220;One particular wave to consider is the Alfven wave, which propagates in magnetized plasmas and has been observed occurring naturally in space.&#8221;</p>
<p>Also listed in the Group 1 category is the &#8220;Atmospheric Breathing Electric Thruster for Planetary Exploration,&#8221; as outlined by Kurt Hohman of Busek Co. Inc.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z24.jpg"><img class="alignleft size-full wp-image-22634" title="Z2" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z24.jpg" alt="" width="350" height="235" /></a>&#8220;This study will investigate the development of an atmosphere‐breathing electric propulsion solar-powered vehicle to explore planets such as Mars. The vehicle would use atmospheric gas for propellant, eliminating the need to launch and carry the propellant from earth. The propulsion thruster would be electric where the gas is ionized in a plasma and accelerated by electromagnetic fields.</p>
<p>&#8220;The combination of high efficiency and high specific impulse of the electric propulsion thruster and free propellant in‐situ will result in an exciting and enabling technology. This could enable NASA to perform missions of extended lifetime and capabilities beyond those available by typical chemical rockets. Phase I will formulate feasibility of the concept through modeling, calculations and preliminary laboratory experiments and push validity into Phase II research.&#8221;</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A42.jpg"><img class="alignleft size-full wp-image-22636" title="A42" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A42.jpg" alt="" width="289" height="335" /></a>Steven Howe, from the Universities Space Research Association, looks back to the heritage of the Apollo missions and <a href="http://www.nasaspaceflight.com/2011/09/voyager-1s-great-escape-search-for-interstellar-space/" target="_blank">deep space exploration probes </a>for his &#8220;Economical Radioisotope Power&#8221; proposal, based around the concept of Radioisotope Thermoelectric Generators (RTGs) to provide electrical power.</p>
<p>&#8220;Almost all robotic space exploration missions, and all Apollo missions to the moon, have used RTGs for electrical power. These RTGs rely on the conversion of the heat produced by the radioactive decay of Pu‐238 to electricity. Unfortunately, the supply of Pu‐238 is about to run out,&#8221; Mr Howe wrote.</p>
<p>&#8220;This study will investigate an economical production method for Pu‐238 that could allow NASA or a private venture to produce several kilograms per year without the need for large government investment.&#8221;</p>
<p>This team is evaluating the production rate in a commercial nuclear reactor, an investigate the optimization of the transit time of the target material in the reactor, for the purpose of experimentally validating this production process and assess its efficiency, and estimate costs for production facilities and handling the waste stream form the process.</p>
<p>Other interesting ideas proposed in Group 1 of the 2011 NIAC effort include &#8220;Metallic Hydrogen: A Game Changing Rocket Propellant&#8221; &#8211; a concept which &#8220;would revolutionize rocketry&#8221;, as introduced by Isaac Silvera of Harvard University.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z44.jpg"><img class="alignleft size-full wp-image-22637" title="Z4" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z44.jpg" alt="" width="349" height="186" /></a>&#8220;Atomic metallic hydrogen, if metastable at ambient pressure and temperature could be used as the most powerful chemical rocket fuel, as the atoms recombine to form molecular hydrogen. This light‐weight high‐energy density material would revolutionize rocketry, allowing single‐stage rockets to enter orbit and chemically fueled rockets to explore our solar system.</p>
<p>&#8220;To transform solid molecular hydrogen to metallic hydrogen requires extreme high pressures, but has not yet been accomplished in the laboratory. The proposed new approach injects electrons into solid hydrogen to lower the critical pressure for transformation. If successful the metastability properties of hydrogen will be studied. This approach may scale down the pressures needed to produce this potentially revolutionary rocket propellant.&#8221;</p>
<p>Often mentioned as a serious contender for future crewed deep space exploration missions, nuclear-related proposals are nothing new. However, per John Slough of MSNW LLC, his &#8220;Nuclear Propulsion Through Direct Conversion of Fusion Energy&#8221; concept is part of the Group 1 proposals.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z51.jpg"><img class="alignleft size-full wp-image-22638" title="Z5" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z51.jpg" alt="" width="350" height="253" /></a>&#8220;The future of manned space exploration and development of space depends critically on the creation of a vastly more efficient propulsion architecture for in‐space transportation. Nuclear-powered rockets can provide the large energy density gain required,&#8221; Mr Slough wrote.</p>
<p>&#8220;A small scale, low cost path to fusion‐based propulsion is to be investigated. It is accomplished by employing the propellant to compress and heat a magnetized plasma to fusion conditions, and thereby channel the fusion energy released into heating only the propellant.</p>
<p>&#8220;Passage of the hot propellant through a magnetic nozzle rapidly converts this thermal energy into both directed (propulsive) energy and electrical energy.&#8221;</p>
<p>Alfonso Tarditi of the University of Houston at Clear Lake also lists a fusion based concept via his &#8220;Aneutronic Fusion Spacecraft Architecture&#8221;, which he claims could drastically change the potential for human and robotic space exploration.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z61.jpg"><img class="alignleft size-full wp-image-22639" title="Z6" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z61.jpg" alt="" width="350" height="239" /></a>&#8220;The proposed design is based on neutron‐free nuclear fusion as the primary energy source. An innovative beam conditioning/ nozzle concept enables useful propulsive thrust directly from the fusion products, while some fraction of the energy is extracted via direct conversion into electricity for use in the reactor and spacecraft&#8217;s systems.</p>
<p>&#8220;This study focuses on providing the framework required to make fusion propulsion an appealing proposition for long‐range space travel (by integrating the power generation and propulsion systems) rather than on the development of a specific fusion reactor concept.</p>
<p>&#8220;However, the scope of this study is not constrained by the immediate availability of fusion energy since it also analyzes &#8220;hybrid&#8221; schemes with a solar or fission primary energy source along with a sub‐critical fusion reactor used as a plasma space propulsion system.&#8221;</p>
<p>On the nuclear fission side of the NIAC supported concepts, Robert Werka &#8211; of the NASA Marshall Space Flight Center (MSFC) &#8211; proposes &#8220;a Concept Assessment of a Fission Fragment Rocket Engine (FFRE) Propelled Spacecraft, which has a safety bonus of enabling the reactor to be charged after arrival in LEO.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z71.jpg"><img class="alignleft size-full wp-image-22640" title="Z7" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z71.jpg" alt="" width="347" height="174" /></a>&#8220;A new technology, the Fission Fragment Rocket Engine (FFRE), requires small amounts of readily available, energy dense, long lasting fuel, significant thrust at specific impulse of a million seconds, and increases safety by charging the reactor after arrival in LEO. If this study shows the FFRE potential, the return could be immense through savings in travel time, payload fraction, launch vehicle support and safety for deep space exploration.</p>
<p>&#8220;Nuclear fission emits charged fission fragments that travel at more than 4 percent of light speed. These normally quickly collide with other atoms in the core. But an FFRE with a magnetically contained dusty plasma core could employ electrical collimation of the charged fragments into an exhaust beam.&#8221;</p>
<p><a href="http://www.nasaspaceflight.com/2010/11/live-minotaur-launch-multiple-satellites/" target="_blank">Solar Sails are also a well-publicized concept</a>, though not usually in the realm of interplanetary exploration. Grover Swartzlander of the Rochester Institute of Technology has proposed a concept which utilizes &#8220;optical lift&#8221; to enhance space missions employing solar sails.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z81.jpg"><img class="alignleft size-full wp-image-22641" title="Z8" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z81.jpg" alt="" width="350" height="254" /></a>&#8220;Although light is massless, it carries momentum. That momentum can be imparted to refracting, reflecting, and absorbing objects in the form of &#8220;radiation pressure&#8221;. Over time, the small but constant supply of radiation pressure may outweigh the large but brief force afforded by conventional propellants,&#8221; wrote Mr Swartzlander.</p>
<p>&#8220;The study team found that transparent refractive objects may settle into a position where they feel a force that is perpendicular to the incoming light direction, akin to the lift experienced by an airplane wing. This study will explore the potential for &#8220;optical lift&#8221; to enhance space missions employing solar sails.</p>
<p>&#8220;Space‐related applications of a fully maneuverable solar craft are numerous. In the distant future, one can imagine interplanetary missions and visits to exoplanets benefiting from the advantages of the optical lift force.&#8221;</p>
<p>Next up for NIAC is the 2012 Spring Symposium, which is being planned for March 27-29, 2012, at the Westin Hotel in Pasadena, California. Current NIAC Fellows &#8211; as listed above &#8211; will attend and give presentations about their Phase I research. The conference will feature exciting keynote speakers and information about NIAC&#8217;s program status and plans.</p>
<p>This will be followed by the first NIAC Phase II NASA Research Announcement, which will be released in early April, 2012.</p>
<p>(Images via NASA, NIAC and L2).</p>
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		<title>SLS capability touted for Europa Lander capability, Enceladus sample return</title>
		<link>http://www.nasaspaceflight.com/2012/01/sls-capability-europa-lander-capability-enceladus-sample-return/</link>
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		<pubDate>Fri, 06 Jan 2012 13:23:18 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
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		<description><![CDATA[As the Space Launch System (SLS) teams head into their first full year since the vehicle was finally announced, fascinating &#8211; albeit well into the future &#8211; Exploration Systems Development (ESD) Design Reference Mission (DRM) options for deep space have been outlined in the SLS Concept Of Operations (Con Ops), options which include ambitious missions [...]


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			<content:encoded><![CDATA[<p>As the Space Launch System (SLS) teams head into their first full year since the vehicle was finally announced, fascinating &#8211; albeit well into the future &#8211; Exploration Systems Development (ESD) Design Reference Mission (DRM) options for deep space have been outlined in the SLS Concept Of Operations (Con Ops), options which include ambitious missions to the moons of Jupiter and Saturn.</p>
<p><span id="more-22583"></span><strong>SLS in 2012:</strong></p>
<p>A solidified version of the roadmap for the Space Launch System (SLS) is expected this year, as much as there had been hoped the details would be forthcoming in the last few months. One of the main challenges is believed to be the long-term funding situation for NASA, which is &#8211; as always &#8211; under pressure.</p>
<p>Such funding constraints on the Agency may even impact on the very configuration of the SLS, although seasoned NASA teams are understood to be providing a level of mitigation by working flexible options on the launch infrastructure.</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?board=37.0">SLS/HLV Forum Section</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=48.0">L2 SLS Section</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div>
<p>However, it was the ever changing refinements to the <a href="http://www.nasaspaceflight.com/2010/03/constellation-pdr-strict-commercial-requirements/" target="_blank">Constellation Program (CxP) vehicles &#8211; again via funding challenges &#8211; which eventually led to schedule milestone slips</a>, the threat of extra costs as a result, all culminating in its cancellation after the findings of the Augustine Commission into Human Space Flight noted that while the vehicle hardware design was sound, billions of extra dollars were <a href="http://www.nasaspaceflight.com/2009/04/refining-constellations-roadmap-2015-hanley-proposes-major-changes/" target="_blank">required to bring the program back into a viable schedule</a>.</p>
<p>The lack of a definitive roadmap &#8211; regardless of the reasons &#8211; is a problem, one which allows for the charge the vehicle should have been designed for the payloads, not the other way around. Such an issue is mitigated to a point by the size of the vehicle, with SLS&#8217; massive capability &#8211; even prior to the evolved 130mt capacity &#8211; allowing for confidence in being able to achieve a large range of missions.</p>
<p><a href="http://www.nasaspaceflight.com/2011/09/sls-finally-announced-nasa-forward-path/" target="_blank">With a solid plan to start with a 70mt capable Block 1 SLS</a>, the Orion (MPCV &#8211; Multi-Purpose Crew vehicle) no longer has the mass constraints it <a href="http://www.nasaspaceflight.com/2008/09/orions-plea-to-ares-i-stop-adversely-hindering-our-design-process/" target="_blank">complained about during its development to launch with the Ares I launch vehicle</a>.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A61.jpg"><img class="alignleft size-full wp-image-22586" title="A61" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A61.jpg" alt="" width="351" height="303" /></a><a href="http://www.nasaspaceflight.com/2011/10/sls-trades-opening-four-rs-25s-core-stage/" target="_blank">By the early 2020s, SLS will be upgraded into the Block 1A configuration</a>, a 100mt vehicle which will utilize either solid or liquid boosters, prior to the eventual Block 2, 130mt vehicle, boosted by its triple J-2X Upper Stage.</p>
<p>All three versions of the SLS will have a crew and/or cargo launch option, <a href="http://www.nasaspaceflight.com/2011/12/building-roadmap-sls-con-ops-lays-leolunar-options/" target="_blank">with the debut uncrewed launch around the Moon, set for 2017, to be followed by the first manned flight, which managers are continuing to push for a 2019 launch date</a> &#8211; a <a href="http://www.nasaspaceflight.com/2011/07/preliminary-nasa-evolved-sls-vehicle-21-years-away/" target="_blank">two year improvement on the &#8220;worst case&#8221; manifest</a>.</p>
<p>This baseline knowledge had provided an initial &#8220;bible&#8221; of operations for the SLS &#8211; known as the info-heavy Concept Of Operations (Con Ops) presentation (<a href="http://forum.nasaspaceflight.com/index.php?topic=27305.0" target="_blank">available in L2</a>), with its content being serialized by this site.</p>
<p>*<a href="http://forum.nasaspaceflight.com/index.php?topic=27423.0" target="_blank">Click here for SLS Con Ops Article List</a>*</p>
<p><strong>SLS Mission Ability &#8211; PART TWO: (<a href="http://www.nasaspaceflight.com/2011/12/building-roadmap-sls-con-ops-lays-leolunar-options/" target="_blank">Click here for Part 1</a>)</strong></p>
<p>Transporting humans further than the Moon has been an ambition of mankind for decades, but something yet to be achieved, not least due to the massive challenge of sustaining a crew on a deep space voyage for many months.</p>
<p>Important lessons are being provided <a href="http://www.nasaspaceflight.com/tag/iss/" target="_blank">by the crews of the International Space Station</a> (ISS), with average tours of six months showing humans can live and work safely &#8220;off planet&#8221; in micro G conditions.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z131.jpg"><img class="alignleft size-full wp-image-22590" title="Z131" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z131.jpg" alt="" width="347" height="257" /></a>However, the ISS is an expertly controlled laboratory, racing around in Low Earth Orbit (LEO), with immediate means of evacuating crewmembers back to the planet if required. Sending humans into deep space, on a relatively small vehicle, will require advances in life support and additional mitigation against critical &#8211; mission ending &#8211; failures, to name but a few of the challenges.</p>
<p>Preliminary work continues to mature on the ground, while teams plan out the potential missions NASA crews will undertake in what will be the next big drive for the Agency, <a href="http://www.nasaspaceflight.com/2011/10/sls-flexibility-roadmap-focus-center-stage/" target="_blank">the return to exploration</a>.</p>
<p>With a return to the Moon &#8211; at least its orbit, but potentially back to the surface &#8211; part of the opening salvo of mission goals for SLS and Orion, the ultimate aim is to send humans to Mars. Such a mission is highly unlikely to take place ahead of the 2030s, meaning NASA may even be beaten by one of the commercial companies &#8211; <a href="http://forum.nasaspaceflight.com/index.php?topic=26269.0" target="_blank">such as SpaceX.<br />
</a><br />
However, providing the tools of being able to successfully send crews as far as Mars will come via interim experience, gained from the initial SLS/Orion missions to the Moon and potentially a Near Earth Object (NEO), more commonly and specifically known as a Near Earth Asteroid (NEA) mission.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A1110A1.jpg"><img class="alignleft size-full wp-image-22591" title="A1110A1" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A1110A1.jpg" alt="" width="350" height="220" /></a>A large amount of training for such a mission has already taken place on Earth, <a href="http://www.nasaspaceflight.com/2011/10/neemo-13-days-underwater-mission-sim-neo-exploration/" target="_blank">not least via the NASA Extreme Environment Mission Operations (NEEMO) missions</a>, which <a href="http://www.nasaspaceflight.com/2011/10/neemo-mission-ends-six-successful-underwater-evas/" target="_blank">recently completed a six-EVA underwater simulation mimicking exploration of an asteroid</a> &#8211; at least from the standpoint of being at the destination, as opposed to the challenge of the transit to and from the NEO.</p>
<p>Cited as the Deep Space (Strategic and Architecture Timeframes) in the expansive Con Ops presentation, missions to NEOs may not require the full Block 2 capability of the SLS &#8211; if NASA managers opted to use the initial mission capability. The larger SLS would be required for an advanced mission profile.</p>
<p>&#8220;The deep space missions are the longest duration missions in the DRM set. These include initial, advanced, and full capability missions to NEA (DRM IDs: NEA_MIN _1A1A/2A_C11B1 and NEA_FUL_1A_C11B1,&#8221; noted the Con Ops presentation.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z41.jpg"><img class="alignleft size-full wp-image-22592" title="Z41" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z41.jpg" alt="" width="350" height="235" /></a>&#8220;The initial capability NEA mission, which is a Strategic timeframe DRM, will require two SLS launches with mass to orbit of approximately 85t and 90t.</p>
<p>&#8220;The advanced capability NEA mission, which is an Architecture timeframe DRM, will require three SLS launches with mass to orbit of approximately 90t, 111t, and 111t.</p>
<p>&#8220;The full capability NEA mission, which is also an Architecture timeframe DRM, requires three SLS launches with lift-off masses of approximately 105t. Each of these missions will require launches spaced 180 days apart.&#8221;</p>
<p>Destination options are not listed in the Con Ops, with the older Flexible Path presentation (<a href="http://forum.nasaspaceflight.com/index.php?topic=19892.0" target="_blank">available in L2</a>) still <a href="http://www.nasaspaceflight.com/2010/01/nasas-flexible-path-2025-human-mission-visit-asteroid/" target="_blank">the most comprehensive overview for the NEA and Mars mission options</a>.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A164.jpg"><img class="alignleft size-full wp-image-22593" title="A164" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A164.jpg" alt="" width="341" height="250" /></a>The most likely candidates cited in the Flexible Path approach include a mission to Near Earth Object 1999AO10, requiring a launch date of January 2, 2026. <a href="http://www.nasaspaceflight.com/tag/neo/" target="_blank">NASA managers continue to note that a NEO mission would likely occur in the middle of the next decade, making this target a viable example</a>.</p>
<p>This deep space mission would last 155 days, around half of the mission length for the other candidate mentioned &#8211; 304 days &#8211; for NEO 2001 GP2.</p>
<p>With a robotic precursor mission launched four years in advance, the 1999AO10 mission is portrayed as requiring two Space Launch System vehicles being readied to launch.</p>
<p>The first HLV launch &#8211; per the Flexible Path approach &#8211; would place the Earth Departure Stage (EDS) and an &#8220;inflatable design Habitat&#8221; &#8211; otherwise known as the Deep Space Hab (DSH) into orbit first.</p>
<p>The higher propellant load Orion/SM (Service Module) &#8211; and likely the MMSEV (Multi Mission Space Exploration Vehicle) &#8211; would then placed in LEO on the second launch. This is a different sequence to that proposed in other presentations, showing how such mission sequences remain undefined at this time.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z22.jpg"><img class="alignleft size-full wp-image-22594" title="Z22" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z22.jpg" alt="" width="351" height="230" /></a>Further information became available <a href="http://www.nasaspaceflight.com/2011/12/asteroid-missions-proving-grounds-future-crewed-mars-missions/" target="_blank">via the Human Space Exploration Community&#8217;s Workshop, under the tagline &#8220;Mission Scenario: Asteroid Next&#8221;, </a>which points to a potential requirement for crewed missions to an Exploration Test Module in the initial years of the 2020 decade.</p>
<p>As referenced by the &#8220;Asteroid Next&#8221; presentation, these mission would be &#8220;In-space habitation for long durations in the appropriate radiation environment&#8221; to gain further knowledge and information on &#8220;radiation protection and measurement techniques; demonstration of beyond Low Earth Orbit re-entry speeds; subsystem high reliability and commonality (and) repair at the lowest level (while) living without a supply chain&#8221; &#8211; something which is extremely important for eventual multi-month/year missions away from Earth.</p>
<p>Under such a scenario, the Exploration Test Module would quickly be replaced by the Deep Space Habitat (DSH) to be launched by the SLS and delivered to the Earth-Moon 1 Lagrange point &#8211; which gives the added benefit of practising operations in a gravitationally null point in the Earth-Moon system.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z311.jpg"><img class="alignleft size-full wp-image-22595" title="Z31" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z311.jpg" alt="" width="350" height="282" /></a>For the DSH, a total of six crewed mission would be planned. While the missions would be tailored in terms of duration to fit specific mission requirements, opening assessments point to an initial 2023 flight to the DSH lasting 14 days with 4 crew members.</p>
<p>This would be followed by an un-crewed resupply mission to DSH by the SLS rocket in preparation for a second crewed mission the following year. This second crewed mission would also fly with 4 people and last for 30 days. The third mission would be flown a year after the second and consist of a 60-day mission with four crewmembers.</p>
<p>The next year would see a four-person crew staying for 90 days at the DSH before a 180-day mission the following year. By which time, a mission to an actual NEA would effectively be practised and proven from a crew survival standpoint.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A57.jpg"><img class="alignleft size-full wp-image-22600" title="A57" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A57.jpg" alt="" width="318" height="245" /></a>This also shows why Mars is so far away from being fully planned, as these precursor missions to the big prize learn mankind how to safely carry out crewed deep space missions, especially in such a risk advise era when compared to the Apollo era.</p>
<p>As outlined previously numerous times, the current favored approach is <a href="http://www.nasaspaceflight.com/2010/01/taking-aim-phobos-nasa-flexible-path-precursor-mars/" target="_blank">to aim for the moon of Phobos as a stepping stone to actually landing on Mars. This mission, while expansively covered in the Flexible Path approach</a>, remains highly notional, given the lack of experience with the initial deep space missions.</p>
<p>However, the Con Ops presentation then provides a surprise, by refocusing on SLS&#8217; unmanned capability, in turn removing the caveat of having to learn how to keep a crew alive during long duration flight.</p>
<p><strong>Missions to Europa and Enceladus:</strong></p>
<p>NASA&#8217;s experience with deep space probes is well known and largely successful, but the Con Ops presentation points to a large advantage that can be gained by their monster rocket &#8211; providing &#8220;direct&#8221; missions to destinations in our solar system, removing the longer transit times that require gravity assists, in turn increasing the mission goals for the passenger payload/spacecraft.</p>
<p>&#8220;The SLS is a feasible option to launch demanding missions to explore the solar system. The SLS capabilities provide three main advantages to Science Payloads: higher energy, larger diameters, and larger mass,&#8221; added the presentation.</p>
<p>For SLS/HLV Articles, click here: <a href="http://www.nasaspaceflight.com/tag/hlv/">http://www.nasaspaceflight.com/tag/hlv/</a></p>
<p>&#8220;The SLS can fly large or medium class payloads to higher energy orbits. This potentially enables direct missions to the outer planets that are currently only achievable using indirect flights with gravity-assist trajectories. An SLS could enable these missions using direct flights with shorter interplanetary transfer times, which enables extensive in situ investigations and potentially sample return options.&#8221;</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A7111.jpg"><img class="alignleft size-full wp-image-22596" title="A7111" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A7111.jpg" alt="" width="348" height="298" /></a>The claim is a fair one when comparing SLS to the currently favored Delta II and <a href="http://www.nasaspaceflight.com/2011/08/ula-atlasv-nasa-juno-jupiter/" target="_blank">Atlas V launch vehicles for such missions involving deep space spacecraft</a>, as SLS&#8217; superior launch mass capability and larger fairing offer exciting possibilities for more ambitious hardware which may be too large for the medium launchers.</p>
<p>&#8220;The SLS also provides 8.4 m and 10.0 m fairings to launch payloads with larger diameter apertures. This capability allows Earth observing, astronomical missions (e.g., planet finders), etc., with the ability to launch large single mirrors and lenses without the expense, complexity, and mass of segmented optics,&#8221; noted the Con Ops presentation.<br />
 <br />
&#8220;The SLS provides a heavy-lift capacity, allowing complex spacecraft to be launched with much higher masses. The large payload capacity of the SLS permits the addition of extra fuel for propulsive maneuvers, shielding to protect from harsh radiation, drill strings and casings for drilling, and redundancy. Sample return missions benefit from all aspects of the SLS performance.&#8221;</p>
<p>As if to drive the point home, the presentation provides examples of such mission capabilities, pointing towards missions to the exciting moons of Jupiter and Saturn, namely Europa and Enceladus.</p>
<p>Europa, is the sixth closest moon of the planet Jupiter, and the smallest of its four Galilean satellites. A water ocean exists beneath its surface, which could conceivably serve as an abode for extraterrestrial life.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z7.jpg"><img class="alignleft size-full wp-image-22597" title="Z7" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z7.jpg" alt="" width="348" height="230" /></a>Sister crafts Pioneer 10 and Pioneer 11 were the first to visit Jupiter, in 1973 and 1974, respectively. <a href="http://www.nasaspaceflight.com/?s=Voyager" target="_blank">The two Voyager probes travelled through the Jovian system in 1979 providing more detailed images of Europa&#8217;s icy surface</a>.</p>
<p>Starting in 1995, Galileo began a Jupiter orbiting mission that lasted for eight years, until 2003. New Horizons imaged Europa in 2007, as it flew by the Jovian system while on its way to Pluto.</p>
<p>The Jupiter Europa Orbiter, as part of the Europa Jupiter System Mission (EJSM) &#8211; a joint NASA/ESA proposal &#8211; is a potential future exploration of Jupiter&#8217;s moons targeting a launch in 2020, <a href="http://www.nasaspaceflight.com/2011/08/ula-atlasv-nasa-juno-jupiter/" target="_blank">while Juno &#8211; launched by an Atlas V - is enroute</a>.</p>
<p>&#8220;The SLS could potentially enable sample return from Jupiter&#8217;s moon Europa, because it would have the payload capacity to provide shielding for a lander on the surface, and sufficient fuel for propulsive maneuvers out of the gravitational well of Jupiter,&#8221; noted the Con Ops presentation.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z8.jpg"><img class="alignleft size-full wp-image-22598" title="Z8" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/Z8.jpg" alt="" width="349" height="243" /></a>&#8220;At Enceladus, a small active moon of Saturn, the SLS could carry the fuel needed to slow down for sample capture from the plumes on Enceladus, or create an artificial plume on either Europa or Enceladus by firing a copper projectile at the surface.&#8221;</p>
<p>Enceladus is the sixth-largest of the moons of Saturn and  one of only three outer solar system bodies (along with Jupiter&#8217;s moon Io and Neptune&#8217;s moon Triton) where active eruptions have been observed.</p>
<p>It has been reported that analysis of the outgassing suggests that it originates from a body of sub-surface liquid water, which along with the unique chemistry found in the plume, has fueled speculations that Enceladus may be the most habitable spot beyond Earth in the Solar System for life.</p>
<p>Most of the data and photography from visiting spacecraft has been acquired by the Voyager 2 and Cassini spacecrafts.</p>
<p>No firm plans to return to the moon have been confirmed, with the Titan Saturn System Mission (TSSM) &#8211; a joint NASA/ESA proposal for exploration of Saturn&#8217;s moons, including Enceladus &#8211; currently behind the Jupiter EJSM in the mission order.</p>
<p>Numerous articles on SLS/Orion and Exploration Roadmaps will be published over the coming weeks and months.<br />
&#8211;<br />
Please note: Clickable links with (L2) references point directly to cited L2 content. Such content is only available to L2 members (please ensure you are logged in). All other clickable links point to NSF articles and open content.</p>
<p>Images: Via L2 content, driven by L2′s fast exapanding SLS specific L2 section, which includes, presentations, videos, graphics and internal updates on the SLS and HLV, available on no other site. Other images via NASA.)</p>
<p>(L2 is – as it has been for the past several years – providing full exclusive SLS coverage, available no where else on the internet. To join L2, click here: <a href="http://www.nasaspaceflight.com/l2/">http://www.nasaspaceflight.com/l2/</a>)</p>
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		<title>GRAIL twins successfully arrive in Lunar Orbit</title>
		<link>http://www.nasaspaceflight.com/2012/01/grail-twins-arrive-in-lunar-orbit/</link>
		<comments>http://www.nasaspaceflight.com/2012/01/grail-twins-arrive-in-lunar-orbit/#comments</comments>
		<pubDate>Mon, 02 Jan 2012 01:40:10 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
				<category><![CDATA[Unmanned]]></category>
		<category><![CDATA[GRAIL]]></category>
		<category><![CDATA[Moon]]></category>

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		<description><![CDATA[NASA&#8217;s two Gravity Recovery And Interior Laboratory (GRAIL) spacecraft have successfully completed their planned main engine burn and have arrived in lunar orbit. GRAIL-A and GRAIL-B will study the moon to yield a better understanding of the internal structure and thermal evolution. This will allow scientists to formulate a model of the Moon&#8217;s formation which [...]


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</ol>]]></description>
			<content:encoded><![CDATA[<p>NASA&#8217;s two Gravity Recovery And Interior Laboratory (GRAIL) spacecraft have successfully completed their planned main engine burn and have arrived in lunar orbit. GRAIL-A and GRAIL-B will study the moon to yield a better understanding of the internal structure and thermal evolution. This will allow scientists to formulate a model of the Moon&#8217;s formation which can also be applied to terrestrial planets.</p>
<p><span id="more-22543"></span><strong>GRAIL Arrival:</strong></p>
<p>GRAIL-B achieved lunar orbit at 2:43 p.m. PST (5:43 p.m. EST) on Sunday, which completed the insertion of the spacecraft, after GRAIL-A successfully completed its burn at 2 p.m. PST (5 p.m. EST) the previous day.</p>
<p>The insertion maneuvers placed the spacecraft into a near-polar, elliptical orbit with an orbital period of approximately 11.5 hours.</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?topic=12921.0">Delta II/GRAIL UPDATES</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?topic=26609.0">L2 Delta II/GRAIL</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div>
<p>Over the coming weeks, the GRAIL team will execute a series of burns with each spacecraft to reduce their orbital period to just under two hours. At the start of the science phase in March 2012, the two GRAILs will be in a near-polar, near-circular orbit with an altitude of about 34 miles (55 kilometers).</p>
<p>Their successful arrival followed a <a href="http://www.nasaspaceflight.com/2011/09/live-ula-deltaii-launch-grail-spacecraft-to-moon/" target="_blank">smooth launch via the 150th flight of the Delta II launch vehicle, which lifted off from SLC-17B at 09:08 Eastern on September 10, 2011</a>.</p>
<p>Shortly after launch, the GRAIL spacecraft deployed their solar arrays as they passed into sunlight for the first time since separating from their carrier rocket. The transit for the GRAIL to the Moon involved a low-energy trajectory, via the Sun-Earth Lagrange 1 point (L1).</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/W2.jpg"><img class="alignleft size-full wp-image-22545" title="W2" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/W2.jpg" alt="" width="347" height="239" /></a>The spacecraft then had the key event of firing their main engines to enter a selenocentric, or lunar, orbit &#8211; as was carried out without issue. The spacecraft will subsequently manoeuvre into lower orbits, before they are moved into formation to begin collecting scientific data.</p>
<p>At the start of the scientific phase of the mission, the spacecraft will be in circular orbits at an altitude of 55 kilometres. Scientific operations are expected to commence on 8 March next year, and last for 82 days. Decommissioning of the spacecraft will begin on 29 May, and the spacecraft are expected to impact the lunar surface in June.</p>
<p>&#8220;NASA greets the new year with a new mission of exploration,&#8221; said NASA Administrator Charles Bolden. &#8220;The twin GRAIL spacecraft will vastly expand our knowledge of our moon and the evolution of our own planet. We begin this year reminding people around the world that NASA does big, bold things in order to reach for new heights and reveal the unknown.&#8221;</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/W3.jpg"><img class="alignleft size-full wp-image-22546" title="W3" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/W3.jpg" alt="" width="350" height="293" /></a>The GRAIL mission being flown as part of NASA&#8217;s Discovery program, which was started in 1992. Discovery is a medium-class programme intended to study the Solar system. many of NASA&#8217;s recent planetary missions have been conducted as part of it.</p>
<p>The principal scientific objectives of the GRAIL mission are to produce a map of the Moon&#8217;s lithosphere, to allow scientists to understand the Moon&#8217;s thermal evolution, and the evolution of breccia within the Moon&#8217;s crust, and to determine more details of the interior, particularly the size of the core, and the structure beneath impact basins.</p>
<p>The two spacecraft are identical, apart from the positioning of star trackers and instruments to allow the spacecraft to fly with their antennae pointing towards each other. They were built by Lockheed Martin, based around a bus developed for the USA-165, or XSS-11, satellite; a technology demonstration spacecraft operated by NASA and the United States Air Force, which was launched in 2005. Each GRAIL spacecraft has a mass of 307 kilograms, including 106 kilograms of hydrazine fuel.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A411.jpg"><img class="alignleft size-full wp-image-22547" title="A411" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/A411.jpg" alt="" width="333" height="349" /></a>The spacecraft are each equipped with two 1.9 square metre, 520-cell, solar arrays, which will generate at least 700 watts of power. The solar arrays will charge a 30 amp-hour lithium ion battery in each spacecraft, which will be used to store power for when the spacecraft are not in sunlight. Propulsion of each spacecraft will be provided by an MR-106L monopropellant engine, capable of generating 22 newtons of thrust.</p>
<p>The spacecraft are three-axis stabilised, with reaction wheels and eight warm gas thrusters, each capable of producing 0.9 newtons of thrust, being used aboard each spacecraft for attitude control. Sun and star trackers and inertial measurement units will allow the spacecraft to determine their orientation. The spacecraft carry avionics systems which are derived from those developed for the Mars Reconnaissance Orbiter, which was launched in 2005.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/W4.jpg"><img class="alignleft size-full wp-image-22548" title="W4" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/W4.jpg" alt="" width="351" height="244" /></a>Each spacecraft carries two transponders operating in the IEEE S band (NATO E band), which will be used to relay data to the ground and to upload commands to the spacecraft. A further S band transponder, the Time-Transfer Assembly, will be used to transmit signals between the spacecraft to synchronise their onboard chronometers.</p>
<p>Two IEEE X band (NATO I or J band) transponders, the Radio Science Beacon, will be used to transmit signals to Earth for Doppler ranging. Finally an IEEE Ka band (NATO K band) transponder, the Microwave Assembly, will be used to find the distance between the two spacecraft, and track their relative motion.</p>
<p>The Ka band transponder forms part of the Lunar Gravity Ranging System or LGRS, which is GRAIL&#8217;s primary instrument. LGRS consists of four elements; the Ultra-Stable Oscillator, or USO, will be used to generate an oscillating signal to synchronise the instruments. This signal will then be transmitted through both the Microwave Assembly (MWA) and Time-Transfer Assembly (TTA) antennae.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/W5.jpg"><img class="alignleft size-full wp-image-22549" title="W5" src="http://www.nasaspaceflight.com/wp-content/uploads/2012/01/W5.jpg" alt="" width="347" height="284" /></a>TTA broadcasts the signal as a ranging code, similar to those transmitted by Global Positioning Satellites. Finally, the data is collected by the Gravity Recovery Processor Assembly, or GPA, which processes it for transmission back to Earth.</p>
<p>LGRS is derived from the K-Band Ranging (KBR) instrument aboard the Gravity Recovery And Climate Experiment, or GRACE, spacecraft, which were launched in March 2002. GRACE, like GRAIL, consists of two spacecraft using radio signals to map the gravitational field, however it is studying Earth&#8217;s gravitational field instead of the Moon&#8217;s.</p>
<p>The two spacecraft also carry the Moon Knowledge Acquired by Middle school students, or MoonKAM, student outreach payload. This will be used to image areas of the Moon at the request of schoolchildren.</p>
<p>A similar programme for Earth imagery, EarthKAM, has been operated aboard the International Space Station since 2001 and also <a href="http://forum.nasaspaceflight.com/index.php?topic=25837.0" target="_blank">flown on Space Shuttle missions STS-89 and STS-99. A prototype, KidSat, was also flown on STS-76, STS-81 and STS-86</a>.</p>
<p>&#8220;I can&#8217;t think of a better way to ring in the New Year than to place two spacecraft into orbit around the moon. Our team is celebrating today,&#8221; said Stu Spath, GRAIL program manager at Lockheed Martin Space Systems Company. &#8220;We used the moon&#8217;s gravity to capture the two GRAIL spacecraft into orbit, and now the science team is going to analyze that same gravitational field to an extraordinary level.&#8221;</p>
<p>(Images via NASA and ULA).</p>
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<p>Related posts:<ol><li><a href='http://www.nasaspaceflight.com/2011/09/live-ula-deltaii-launch-grail-spacecraft-to-moon/' rel='bookmark' title='Permanent Link: Delta II launches with moon-bound GRAIL spacecraft'>Delta II launches with moon-bound GRAIL spacecraft</a> <small>The Delta II rocket has launched on its 150th flight...</small></li>
<li><a href='http://www.nasaspaceflight.com/2008/10/isro-moon-launch/' rel='bookmark' title='Permanent Link: India launch debut moon mission in collaboration with NASA and ESA'>India launch debut moon mission in collaboration with NASA and ESA</a> <small>The Indian Space Research Organisation (ISRO) has launched their Chandrayaan-1...</small></li>
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		<title>Year in Review &#8211; Part 2: Kepler makes astonishing discoveries</title>
		<link>http://www.nasaspaceflight.com/2011/12/year-in-review-r2-kepler-astonishing-discoveries/</link>
		<comments>http://www.nasaspaceflight.com/2011/12/year-in-review-r2-kepler-astonishing-discoveries/#comments</comments>
		<pubDate>Thu, 29 Dec 2011 22:18:29 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
				<category><![CDATA[Featured]]></category>
		<category><![CDATA[Other]]></category>
		<category><![CDATA[Unmanned]]></category>
		<category><![CDATA[Kepler]]></category>

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		<description><![CDATA[Following on the planetary accomplishments of NASA&#8217;s fleet of unmanned solar system explorers in 2011, the U.S. space agency was also extremely busy in the field of extra-solar studies via observations of other solar systems with the impressive Kepler Space Telescope. Understanding our uniqueness - Kepler sheds light on extra-solar planets: It was a difficult start [...]


Related posts:<ol><li><a href='http://www.nasaspaceflight.com/2009/03/live-delta-ii-set-for-kepler-planet-finder-launch/' rel='bookmark' title='Permanent Link: Delta II launches with Kepler Planet-Finder Launch'>Delta II launches with Kepler Planet-Finder Launch</a> <small>The Delta II launch team at the Cape Canaveral Air...</small></li>
</ol>]]></description>
			<content:encoded><![CDATA[<p>Following on the planetary accomplishments of NASA&#8217;s fleet of unmanned solar system explorers in 2011, the U.S. space agency was also extremely busy in the field of extra-solar studies via observations of other solar systems with the impressive Kepler Space Telescope.</p>
<p><span id="more-22462"></span><strong>Understanding our uniqueness - Kepler sheds light on extra-solar planets:</strong></p>
<p>It was a difficult start to 2011 for the Kepler team. Beginning the year with an anomaly resolution stemming from the spacecraft putting itself into safe mode on December 22, 2010, the Kepler project team successfully returned the spacecraft to normal operations on January 6, 2011 after determining that the condition was caused by an &#8220;unexpected noise in the signal from Kepler&#8217;s sun sensors that erroneously indicated Kepler might be pointing too close to the sun.&#8221;</p>
<p>It wasn&#8217;t long after this that the Kepler team announced the confirmation of the first discovery of our rocky planet outside of our own solar system.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z215.jpg"><img class="alignleft size-full wp-image-22464" title="Z2" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z215.jpg" alt="" width="351" height="254" /></a>The planet, dubbed Kepler-10b, measures 1.4 times the size of Earth and was, at the time, the smallest planet ever discovered outside our own solar system.</p>
<p>While a primary goal of the Kepler mission is to discover rocky planets that lie within the habitable zone of their parent stars, Kepler-10b was quickly dismissed as a habitable candidate because the planet orbits its parent star every 0.84 days, making the planet more than 20 times closer to its star than Mercury is to the sun.</p>
<p>Nevertheless, the discovery of this planet was a proof of concept for the Kepler team, demonstrating that the telescope&#8217;s ultraprecise photometer could in fact measure the tiny decrease in a star&#8217;s brightness that occurs when a small, Earth-sized planet crosses in front of it.</p>
<p>In a statement following this announcement, NASA stated that &#8220;The discovery of Kepler-10b, a bona fide rocky world, is a significant milestone in the search for planets similar to our own.</p>
<p>&#8220;Although this planet is not in the habitable zone, the exciting find showcases the kinds of discoveries made possible by the mission and the promise of many more to come.&#8221;</p>
<p>But this discovery would prove to be just the first of many for Kepler in 2011.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z312.jpg"><img class="alignleft size-full wp-image-22465" title="Z3" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z312.jpg" alt="" width="347" height="255" /></a>One month later, scientists announced the discovery of a six-planet system made up of a mix of rocky and gas giant planets orbiting a single, sun-like star.</p>
<p>Located approximately 2,000 light years from Earth, the Kepler-11 star system was the first such extra-solar planetary system discovered to have more than three confirmed planets.</p>
<p>All the planets discovered in the Kepler-11 system are larger than Earth, with the largest ones comparable to the size of Uranus and Neptune.</p>
<p>The system is extremely compact, with the outermost confirmed planet, Kepler-11g, orbiting its star at a distance twice as close as planet Earth orbits the sun.</p>
<p>The discovery of the system by the Kepler telescope was independently confirmed by ground based observatories as well as the Spitzer Space Telescope.</p>
<p>Moreover, the same day of the announcement of the Kepler &#8211; 11 system also saw the announcement of 54 new planet candidates where their orbits could lie within the habitable zone of their respective parent stars.</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?board=49.0">Space Science Forum</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=35.0">L2 Photo Section</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div>
<p>Since the start of the Kepler mission in March 2009, the number of Earth-sized planet candidates has grown from 0 to 68 while the number of planet candidates in the habitable zone of their parent stars has grown from 0 to 54.</p>
<p>The habitable zone, defined as the region in a planetary system where liquid water could exist on a planetary surface, is of particular interest for the Kepler team in the search for habitable planets like Earth.</p>
<p>But Kepler is not just searching for habitable planets outside our solar system. The telescope is also helping scientists learn more about the stars in our galactic neighborhood.</p>
<p>Following two safe mode events in February and March, NASA announced that the Kepler telescope had aided University of Sydney astrophysicists in their study of red giant stars.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A317.jpg"><img class="alignleft size-full wp-image-22466" title="A317" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A317.jpg" alt="" width="320" height="273" /></a>The study, which revealed new information on the evolution of red giant stars, was aided by the Kepler telescope through the use of its high precision brightness measurements of the various stars in its field of view.</p>
<p>Specifically, Kepler provided scientists a view of hundreds of red giants at a level of precision and duration that ground-based telescopes are not capable of.</p>
<p>Less than two weeks later, further information was revealed about Kepler&#8217;s insight into the study of the internal structure of stars by observing miniscule pulsations in the stars&#8217; brightness.</p>
<p>And still the discoveries kept coming.</p>
<p>By the end of May 2011, Kepler&#8217;s team had found an additional planet in the Kepler-10 system. This confirmed planet, with a radius of 2.2 times that of Earth, completes an orbit of its parent star every 45 days &#8211; making it an extremely hot world that lies too close to its parent star to be habitable.</p>
<p>But perhaps more excitingly by this point in its existence, the Kepler space telescope had identified more than 1,200 planetary candidates, 408 of them residing in planetary systems with two or more planets.</p>
<p>Furthermore, in August of this year, astronomers announced the discovery of the darkest-known exoplanet.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z49.jpg"><img class="alignleft size-full wp-image-22467" title="Z4" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z49.jpg" alt="" width="347" height="295" /></a>Described as a Jupiter-sized gas giant known as TrES-2b, the planet was found to reflect less than 1 percent of the starlight reaching the upper layers of its atmosphere.</p>
<p>While the planet was first discovered using the Trans-Atlantic Exoplanet Survey (TrES) method in 2006, new data from the Kepler telescope allowed scientists to determine the reflectivity of the planet. This led to the discovery that TrES-2b lacks reflective clouds due to its high temperature &#8211; a direct result of its 3-million-distance orbit of its parent star.</p>
<p>This close proximity to its parent star yields an average temperature of 1,800-degrees F, which is too hot for high-reflectivity clouds, like ammonia clouds, to form.</p>
<p>In place of those ammonia clouds, scientists have determined that the atmosphere of this planet contains light absorbing chemicals; however, none of these light absorbing chemicals can fully explain the extreme low-reflectivity of TrES-2b.</p>
<p>Click here for:<br />
*<a href="http://www.nasaspaceflight.com/2009/03/live-delta-ii-set-for-kepler-planet-finder-launch/" target="_blank">Kepler Launch Article</a>*<br />
*<a href="http://www.nasaspaceflight.com/2010/08/kepler-results-ramps-up-search-extra-solar-planets/" target="_blank">Kepler 2010 Review Article</a>*</p>
<p>Moreover, the planet is believed to be tidally locked with its parent star, meaning that one side of the planet always faces the star.</p>
<p>Further observations from the Kepler telescope also showed that the planet has changing phases as it orbits its star, causing the total brightness of the star and its planet to vary slightly during observational periods.</p>
<p>Furthermore, direct observations from Kepler of TrES-2b yielded the detection of the smallest-ever change in brightness from an exoplanet at just six parts per million &#8211; making Kepler the first telescope to detect such a minute change in brightness of an exoplanet.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z55.jpg"><img class="alignleft size-full wp-image-22468" title="Z5" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z55.jpg" alt="" width="350" height="286" /></a>Following this dark world discovery, the Kepler team soon announced the discovery of an invisible world orbiting a sun-like star in the Kepler-19 system, located some 650 light years from Earth in the direction of the constellation Lyra.</p>
<p>The discovery of this invisible world was made possible by direct observations of the planet Kepler-19b which, based on its 8.4 million mile distance from its parent star, should complete an orbit every 9 days and 7 hours.</p>
<p>However, +/- 5 minute variations in the orbital times of Kepler-19b led astronomers to the discovery of the invisible world accompanying Kepler-19b.</p>
<p>As related by Kepler researchers, &#8220;If Kepler-19b were alone, each transit would follow the next like clockwork. Instead, the transits come up to five minutes early or five minutes late. Such transit timing variations show that another world&#8217;s gravity is pulling on Kepler-19b, alternately speeding it up or slowing it down.&#8221;</p>
<p>For context within our own solar system, the planet Neptune was similarly discovered when researchers noticed that Uranus orbit didn&#8217;t match predictions. It was soon understood and that the perturbations in Uranus&#8217; orbit were being caused by an unseen planet at a greater distance from the sun than Uranus.</p>
<p>Ground based telescopes soon discovered Neptune near its predicted position based on the observed perturbations in Uranus&#8217; orbit.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/a26.jpg"><img class="alignleft size-full wp-image-22469" title="a26" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/a26.jpg" alt="" width="320" height="240" /></a>While nothing aside from the gravitationally-mandated existence of the invisible world, named Kepler-19c, is known, observations of the Kepler-19 system indicate that Kepler-19c&#8217;s orbit is tilted relative to Kepler-19b, meaning that the planet does not transit the Kepler-19 star and therefore cannot be directly observed by the Kepler telescope or from ground-based observatories on Earth.</p>
<p>But, like before, the discoveries and confirmations from Kepler just kept coming.</p>
<p>By mid-September, the Kepler team announced the discovery of a planet orbiting a binary star system.</p>
<p>Residing in a star system 200 light years from Earth, the planet, called Kepler-16b, marked the first confirmation of an unambiguous circumbinary planet -  a planet that orbits two stars in the same system.</p>
<p>Demonstrating the diversity of planets within our own galaxy, Kepler-16b is cold and lies outside of its parent stars&#8217; habitable zone.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z65.jpg"><img class="alignleft size-full wp-image-22470" title="Z6" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z65.jpg" alt="" width="349" height="258" /></a>The planet was discovered using the transit method of detection, viewing the relative dimming and brightening of a star (or stars in this case) as a planet passes between the star and Kepler&#8217;s line of sight.</p>
<p>Observations of the stars&#8217; interaction with Kepler-16b confirmed the planet to be roughly the size of Saturn with a rocky and gaseous composition.</p>
<p>The planet was confirmed to orbit the two stars every 229 days, placing it &#8211; if it were in our own solar system &#8211; in nearly the precise orbit of Venus, which takes 225 days to orbit the sun.</p>
<p>However, because the two stars in the Kepler-16 system are cooler than our sun, Kepler-16b in fact lies well beyond the habitable zone of the Kepler 16 system.</p>
<p>Furthermore, by early October, Kepler had aided in the discovery of an &#8220;unusual multi-planet system&#8221; in which a super Earth and two Neptune-size planets all orbit in resonance with each other.</p>
<p>The confirmed three-planet system, if superimposed over a map of our own solar system, would lie complete within the orbit of Mercury. But while all these previous discoveries and confirmations were exciting in their own right, nothing could compare to the final three Kepler announcements of 2011.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z91.jpg"><img class="alignleft size-full wp-image-22473" title="Z9" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z91.jpg" alt="" width="347" height="280" /></a>On December 2, the discovery of a super-Earth was confirmed around one of the brightest stars in Kepler&#8217;s field of view.</p>
<p>Dubbed Kepler-21b, the planet is roughly 1.6 times the size of Earth and 10 times Earth&#8217;s mass.</p>
<p>It orbits its parent star every 2.8 days at a distance of only 6 million kilometers &#8211; ten times closer to its star than Mercury is to the sun.</p>
<p>The surface temperate on Kepler-21b is estimated to be roughly 2,960 degrees F. Thus, the planet does not lie within the habitable zone of its parent star, the habitable zone still only defined as the zone around a star in which liquid water could exits on the surface of a rocky planetary body.</p>
<p>The star itself, HD 179070 is 352 lights years from Earth.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z81.jpg"><img class="alignleft size-full wp-image-22472" title="Z8" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z81.jpg" alt="" width="350" height="268" /></a>But this still could not compare to the announcement that came on December 5: the first confirmed planet to lie within the habitable zone of its parent star &#8211; which is a sun-like star to boot.</p>
<p>The planet, called Kepler 22b, was, as of December 5, the smallest-yet confirmed planet found to orbit completely within the habitable zone of a star similar to the sun &#8211; a G-type star.</p>
<p>The planet lies 600 light years away from Earth and orbits its parent star every 290 days.</p>
<p>At approximately 2.4 times the radius of Earth, Kepler-22b has not yet been confirmed as a rocky planet.</p>
<p>As NASA stated, &#8220;This is a major milestone on the road to finding Earth&#8217;s twin. Kepler&#8217;s results continue to demonstrate the importance of NASA&#8217;s science missions, which aim to answer some of the biggest questions about our place in the universe.&#8221;</p>
<p>At this time, Kepler-22b is the first of 54 habitable zone planet candidates, as reported in February 2011, to be independently confirmed by follow-up observations after its initial discovery.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z73.jpg"><img class="alignleft size-full wp-image-22471" title="Z7" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z73.jpg" alt="" width="346" height="259" /></a>As of December 5, the number of planet candidates from Kepler totaled 2,326 &#8211; up 89 percent from February 2011. Of that number, roughly 207 are Earth-sized planets, 680 are super Earth-sized, 1,181 are Neptune-sized planets, 203 are Jupiter-sized planets, and 55 are larger than Jupiter.</p>
<p> Moreover, the number of habitable zone planet candidates decrease from 54 in February to 48, representing a shift in the definition and placement of the habitable zone around stars to account for atmospheric heating which subsequently moves the habitable zone further out from a star.</p>
<p>But that was not the end for Kepler in 2011. The final announcement came two weeks ago with the confirmation of actual Earth-sized planets.</p>
<p>Kepler-20e and Kepler-20f, lying in a star system approximately 1,000 light years from Earth, orbit a sun-like star.</p>
<p>Most exciting is the small size of these planets, with Kepler-20e being slightly smaller than Venus at 0.87 times the radius of Earth and Kepler-20f being 1.03 times the radius of Earth.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z102.jpg"><img class="alignleft size-full wp-image-22474" title="Z10" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z102.jpg" alt="" width="347" height="245" /></a>Together, these are the two smallest exoplanets yet discovered.</p>
<p>Kepler-20e orbits the host star every 6.1 days while Kepler-20f takes 19.6 days to orbit the star. This places the two worlds too close to their parent star to be habitable by current definitions. If superimposed over our own solar system, the entire five planet system would lie completely within the orbit of Mercury.</p>
<p>In fact, the most-distant confirmed planet in the Kepler-20 system only takes 77.6 days to orbit the star, compared with Mercury&#8217;s 88 day orbital period around the sun.</p>
<p>Furthermore, the Kepler-20 system is helping expand our understanding of the composition of other solar systems in our galactic neighborhood.</p>
<p>While our solar system is arranged with the smallest planets closest to the sun and the largest planets farther away, the Kepler-20 system is arranged in an alternating pattern of large, small, large, small, large &#8211; all and all, an amazing discovery to cap an amazing year for Kepler.</p>
<p>(All images via NASA).</p>
<img src="http://www.nasaspaceflight.com/wp-content/plugins/pixelstats/trackingpixel.php?post_id=22462&amp;ts=1328917967" style="display:none;" alt="pixelstats trackingpixel"/>

<p>Related posts:<ol><li><a href='http://www.nasaspaceflight.com/2009/03/live-delta-ii-set-for-kepler-planet-finder-launch/' rel='bookmark' title='Permanent Link: Delta II launches with Kepler Planet-Finder Launch'>Delta II launches with Kepler Planet-Finder Launch</a> <small>The Delta II launch team at the Cape Canaveral Air...</small></li>
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		<title>Year in Review &#8211; Part 1: NASA&#8217;s planetary probes dominate in 2011</title>
		<link>http://www.nasaspaceflight.com/2011/12/year-in-review-p1-nasas-planetary-probes-dominate-2011/</link>
		<comments>http://www.nasaspaceflight.com/2011/12/year-in-review-p1-nasas-planetary-probes-dominate-2011/#comments</comments>
		<pubDate>Tue, 27 Dec 2011 02:15:58 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
				<category><![CDATA[Featured]]></category>
		<category><![CDATA[Other]]></category>
		<category><![CDATA[Unmanned]]></category>
		<category><![CDATA[Cassini]]></category>
		<category><![CDATA[Dawn]]></category>
		<category><![CDATA[GRAIL]]></category>
		<category><![CDATA[Juno]]></category>
		<category><![CDATA[MESSENGER]]></category>
		<category><![CDATA[Voyager 1]]></category>

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		<description><![CDATA[It was an interesting year for NASA as the 2011 calendar brought about the retirement of the iconic Space Shuttle fleet, the completion of the USOS segment of the International Space Station, the launch of three new planetary missions, and the ongoing scientific endeavors of NASA&#8217;s fleet of planetary probes. In all, 2011 proved a [...]


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			<content:encoded><![CDATA[<p>It was an interesting year for NASA as the 2011 calendar brought about the retirement of the iconic Space Shuttle fleet, the completion of the USOS segment of the International Space Station, the launch of three new planetary missions, and the ongoing scientific endeavors of NASA&#8217;s fleet of planetary probes. In all, 2011 proved a banner year for NASA&#8217;s unmanned explorers in our solar system.</p>
<p><span id="more-22409"></span><strong>Background:</strong></p>
<p>While much of the world&#8217;s attention was on NASA&#8217;s manned exploits in 2011, the US space agency was busy with its fleet of unmanned planetary explorers peppered throughout the inner and outer solar system.</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?board=49.0">Space Science Forum</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=35.0">L2 Photo Section</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=34.0">L2 Historical Section</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div>
<p>In particular, NASA&#8217;s MESSENGER, Dawn, Cassini, and Voyager 1 spacecrafts increased our knowledge of Mercury, the asteroid belt, Saturn, and the outer-most boundary of our solar system, while the intrepid rover Opportunity revealed more secrets about our third closest celestial neighbor: Mars.</p>
<p>Calendar year 2011 for NASA also saw the launch of three new and exciting missions: the twin GRAIL probes to the moon, the Juno spacecraft to the Jupiter, and the Mars Science Laboratory rover Curiosity to Mars.</p>
<p>Sadly, 2011 also brought about the end of official operations for the Mars rover Spirit which survived on the red planet for over six years.</p>
<p><strong>The new missions: GRAIL, Juno, and MSL:</strong></p>
<p>Continuing a string of successes in planetary missions, NASA began three new planetary flights in 2011, including one designed to build the presence of the space agency around the moon.</p>
<p><strong>GRAIL and the new mission to the moon:</strong></p>
<p><a href="http://www.nasaspaceflight.com/2011/09/twin-grail-satellites-ready-for-nasa-lunar-launch/" target="_blank">Dubbed the GRAIL mission, the twin Gravity Recovery And Interior Laboratory spacecraft</a> will be the first of their kind to conduct an unprecedented and detailed study of Earth&#8217;s closest celestial neighbor from the crust of its surface to its inner-most core.</p>
<p><a href="http://www.nasaspaceflight.com/2011/09/live-ula-deltaii-launch-grail-spacecraft-to-moon/" target="_blank"><img class="alignleft size-full wp-image-22412" title="A411" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A4112.jpg" alt="" width="333" height="349" />Launching aboard the veteran Delta II rocket from the Cape Canaveral Air Force Station on Saturday, September 10</a>, the twin spacecraft enjoyed an issue-free 3.5 month low energy transfer cruise to the Moon and are scheduled to arrive in lunar orbit on December 31, 2011 and January 1, 2012.</p>
<p>Powered by a series of solar panels on their surface, NASA hopes that the GRAIL spacecraft will answer longstanding questions about the Moon and give scientists a better understanding of how Earth and other rocky planets in the solar system formed.</p>
<p>Flown under NASA&#8217;s Discovery program, the principle scientific objectives of the GRAIL mission are to produce a map of the moon&#8217;s lithosphere, allow scientists to understand the moon&#8217;s thermal evolution and the evolution of breccia with in the moon&#8217;s crust, and determine more details of the moon&#8217;s interior, particularly the size of the moon&#8217;s core and the structure beneath impact basins.</p>
<p>Once inserted into lunar orbit, the twin GRAIL spacecraft will work in harmony with one another during the primary 82 day scientific collection phase of the mission.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A721.jpg"><img class="alignleft size-full wp-image-22413" title="A72" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A721.jpg" alt="" width="350" height="295" /></a>While nothing beyond the 82-day primary science mission has been confirmed, it is entirely possible &#8211; based on past mission extension operations from NASA &#8211; that the GRAIL mission could enjoy a longer life in orbit of the moon.</p>
<p>However, this mission&#8217;s launch also signaled the apparent end of NASA&#8217;s selection of the Delta II rocket as a preferred launch vehicle.  Following numerous successful flights with Delta II, NASA is now moving in the direction of selecting the Atlas V and Delta IV launch vehicles over the Delta II.</p>
<p>While NASA has publicly expressed optimism that a future mission could utilize the Delta II launch vehicle&#8217;s services, no such official commitment has been made and none of NASA&#8217;s currently planned missions are scheduled to use the Delta II rocket. </p>
<p>Therefore, the launch of the GRAIL spacecrafts marked the penultimate flight of the Delta II, with its final flight occurring in late October, and final time NASA used the veteran rocket. (<a href="http://forum.nasaspaceflight.com/index.php?topic=26609.0" target="_blank">GRAIL L2 Coverage</a>).</p>
<p><strong>Returning to the giant:</strong></p>
<p>Nonetheless, the GRAIL mission was not the first of the new planetary missions launched by NASA in 2011.  Almost exactly one month earlier in early August, NASA successfully launched the new <a href="http://www.nasaspaceflight.com/2005/06/nasa-makes-selection-on-jupiter-mission/" target="_blank">Juno probe to the solar system&#8217;s giant: Jupiter</a>.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z310.jpg"><img class="alignleft size-full wp-image-22418" title="Z3" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z310.jpg" alt="" width="350" height="245" /></a><a href="http://www.nasaspaceflight.com/2011/07/nasa-juno-frr-completed-atlas-delta-share-ride-mariner/" target="_blank">Riding atop the second most powerful configuration for the Atlas V</a> rocket, <a href="http://www.nasaspaceflight.com/2011/08/ula-atlasv-nasa-juno-jupiter/" target="_blank">the Juno mission lifted off at 1225 EDT on 5 August 2011</a> - after a 51 minute delay for a technical issue and a boat in the launch restriction zone. </p>
<p>Since launch, Juno has traveled approximately 221 million miles and has achieved a velocity of 55,800 miles per hour relative to the sun.</p>
<p>Named after the Roman goddess of marriage and the wife of the god Jupiter, the Juno mission is the second mission in NASA&#8217;s New Frontiers program &#8211; the first being the New Horizons probe currently on its way to an encounter with Pluto and its moons in July 2015.</p>
<p>The spacecraft made its first of three Mars orbit crossings on December 13 in anticipation for its August 2016 arrival at Jupiter after a five year trek through the inner and outer solar system. During this five year trek, the spacecraft will make a flyby of Earth in October 2013 for a gravitational assist to propel itself into the outer solar system.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A41.jpg"><img class="alignleft size-full wp-image-22415" title="A41" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A41.jpg" alt="" width="349" height="258" /></a>Once it arrives at Jupiter, Juno will enter a zenocentric orbit of the gas giant for a primary scientific mission that is scheduled to last 14 months and allow the spacecraft to study Jupiter from a polar orbit.</p>
<p>To accomplish this, the Lockheed Martin-built spacecraft will carry nine instruments to Jupiter to study electric currents flowing along field lines in the planet&#8217;s magnetic field, ultraviolet and electromagnetic emissions of the energetic particles in Jupiter&#8217;s aurora, heat being emanated from the planet, the structure of  Jupiter&#8217;s atmosphere, the magnetosphere&#8217;s structure in the planet&#8217;s polar regions, and the energy and distribution of particles and the polar regions of Jupiter&#8217;s magnetosphere.</p>
<p>In all, Juno will be the ninth spacecraft to visit the planet Jupiter, the first being the pioneer 10 spacecraft which flew through the Jovian system in December 1973.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A61.jpg"><img class="alignleft size-full wp-image-22416" title="A61" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A61.jpg" alt="" width="350" height="239" /></a>Juno will be the first spacecraft to be placed into orbit around Jupiter since the Galileo mission which lasted from December 8, 1995 to September 21, 2003.</p>
<p>The connection between Juno to its predecessor Galileo is somewhat ironic to space fans. The Juno mission was in fact the first NASA mission to be launched after the fly out of the Space Shuttle Program.  The final flight of the shuttle program flown by orbiter Atlantis landed just 15 days before Juno&#8217;s launch.  The previous Jovian orbiter mission of Galileo was launched by the very same Space Shuttle &#8211; Atlantis &#8211; in 1989.</p>
<p>Additionally, the successful launch of the Juno mission represented the 175th flight of an Atlas rocket with a Centaur upper stage.  The Atlas-Centaur duo first flew in May 1962 and has since undergone several iterations.</p>
<p>The most current iteration, <a href="http://www.nasaspaceflight.com/2011/11/the-respected-atlas-v-making-early-strides-transition/" target="_blank">the Atlas V rocket, is one of the most reliable U.S. domestic launch vehicles in service today</a>.  At the time of the Juno launch, the Atlas V rocket was in fact the second most reliable U.S. domestic launch vehicle behind only the Delta II rocket &#8211; given that the Shuttle had been retired just 15 days prior.</p>
<p>By late November, when the third of NASA&#8217;s three new planetary missions was launched, the Atlas V was the most reliable U.S. domestic launch vehicle in service following the defacto retirement of the Delta II rocket in late October due to no further customer requests for its services. (<a href="http://forum.nasaspaceflight.com/index.php?topic=26258.0" target="_blank">Juno L2 Coverage</a>).</p>
<p><strong>Mars Science Laboratory - Unlocking the further secrets of Mars:</strong></p>
<p><a href="http://www.nasaspaceflight.com/2011/11/curiosityatlas-v-teams-set-weekend-launch-mars/" target="_blank">NASA&#8217;s third new planetary mission of the year</a> was perhaps the most anticipated of NASA&#8217;s unmanned missions in 2011. </p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z64.jpg"><img class="alignleft size-full wp-image-22419" title="Z6" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z64.jpg" alt="" width="349" height="240" /></a>Carrying the Mars Science Laboratory (MSL) rover Curiosity, the veteran <a href="http://www.nasaspaceflight.com/2011/11/live-atlas-v-launch-nasas-msl-rover-mars/" target="_blank">Atlas V rocket flying on its 28th mission lifted off from the Cape Canaveral Air Force Station at the beginning of a 1 hour 43 minute window at 10:02 EST on 26 November 2011</a>.</p>
<p>For the Atlas V rocket, the launch of Curiosity marked the 28th out of 28 successful missions for the rocket, giving the vehicle, from a payload customer standpoint, a perfect success record.</p>
<p>Successfully sending the MSL rover on its way to the red planet, the Atlas V rocket began what will be a nine month journey through the interplanetary medium for Curiosity.</p>
<p>Scheduled to arrive on 6 August 2012 at approximately 0100 EDT, the MSL will pioneer a new precision landing technology for NASA and a sky-crane touchdown to place Curiosity near the foot of a mountain inside Gale crater.</p>
<p>According to NASA, the new precision landing maneuvers have allowed scientists to shrink the target landing area to less than one-fourth the size of earlier Mars mission landing targets &#8211; a new innovation that without which would have made Gale crater an unacceptably hazardous area for Curiosity to land.</p>
<p>While the primary goal of the MSL mission is to determine whether Mars is or has ever had an environment capable of supporting life, the mission will not look for any specific type of life.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/D27.jpg"><img class="alignleft size-full wp-image-22417" title="D27" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/D27.jpg" alt="" width="352" height="234" /></a>Instead, the rover will use a suite of 10 scientific instruments along with a robotic arm to analyze soil and rock samples with a complex set of laser and sensor systems.</p>
<p>In all, Curiosity is five times larger than its predecessors Spirit and Opportunity and has 15 times the mass of scientific experiments of Spirit and Opportunity.</p>
<p>Curiosity&#8217;s primary science mission phase is scheduled to last 687 Earth days or one Martian year and cover between 5-20 kilometers on Mars&#8217;s surface.</p>
<p>The mission was initially scheduled to launch in the 2009 Martian launch window but was delayed due to inadequate test time and technical and budgetary reasons. (<a href="http://forum.nasaspaceflight.com/index.php?topic=27244.0" target="_blank">MSL L2 Coverage</a>).</p>
<p><strong>NASA&#8217;s ongoing missions - from Mercury to the edge of the solar system:</strong></p>
<p>While the new missions launched by NASA this year certainly offer up the potential to provide intriguing new insights into the solar system and planetary formation, the successes of ongoing NASA missions that are already collecting data on this very topic dominated much of the space community&#8217;s news in 2011.</p>
<p>In fact, 2011 proved to be the year in which two major historic events in the unmanned space probe arena would finally come to fruition: the successful insertion of the MESSENGER probe into orbit around the planet Mercury and a successful orbital insertion of the Dawn spacecraft around the asteroid Vesta.</p>
<p><strong>MESSENGER at Mercury:</strong></p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z72.jpg"><img class="alignleft size-full wp-image-22420" title="Z7" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z72.jpg" alt="" width="349" height="224" /></a>The first of these two major achievements occurred on 17 March 2011 when the MESSENGER spacecraft confirmed its successful orbital insertion of planet Mercury at 2110 EDT.</p>
<p>As related by NASA, &#8220;Achieving Mercury orbit was by far the biggest milestone since MESSENGER was launched more than six and a half years ago. This accomplishment is the fruit of a tremendous amount of labor on the part of the navigation, guidance-and-control, and mission operations teams, who shepherded the spacecraft through its 4.9-billion-mile journey.&#8221;</p>
<p>Within days, MESSENGER had sent back its first image of Mercury from orbit and began what was thought to be a year-long Mercury science mission which was due to end on 17 March 2012.</p>
<p>However, on 14 November 2011, NASA announced the extension of the MESSENGER mission for an additional year of orbital operations at Mercury, ensuring the spacecraft&#8217;s operation, from a funding and ground support stance, through 17 March 2013.</p>
<p>This extension comes in large part due to the tremendous success of the MESSENGER mission in its first six months of operation in orbit of Mercury.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z8.jpg"><img class="alignleft size-full wp-image-22421" title="Z8" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z8.jpg" alt="" width="350" height="271" /></a>So far, MESSENGER has revealed unexpectedly high concentrations of magnesium and calcium on the night time side of Mercury and the offset to the north of the planet&#8217;s center of the magnetic field.</p>
<p>During the first year of its operations, MESSENGERs primary science objectives include determining accurately the surface composition of Mercury, characterizing the geological history of the planet, determing the precise strength of the magnetic field and its variations with position and altitude, investigating the presence of a liquid outer core by measuring Mercury&#8217;s liberation (oscillating motion of orbiting bodies relative to each other), determining the nature of the radar reflective materials at Mercury&#8217;s polls, and investigating the important volatile species and their sources and sinks on and near Mercury.</p>
<p>Following from the primary year of scientific exploration, the one year extension will be designed to explore six scientific questions regarding Mercury.  Specifically these questions include: What are the sources of surface volatiles on Mercury? How late into Mercury&#8217;s history did volcanism persist? How did Mercury&#8217;s long-wavelength topography change with time? What is the origin of localized regions of enhanced exospheric density at Mercury? How does the solar cycle affect Mercury&#8217;s exosphere and volatile transport? And what is the origin of Mercury&#8217;s energetic electrons?</p>
<p>As related by NASA, &#8220;Advancements in science have at their core the evaluation of hypotheses in the light of new knowledge, sometimes resulting in slight changes in course, and other times resulting in paradigm shifts, opening up entirely new vistas of thought and perception.</p>
<p>&#8220;With the early orbital observations at Mercury we are already seeing the beginnings of such advancements. The extended mission guarantees that the best is indeed &#8216;yet to be&#8217; on the MESSENGER mission, as this old-world Mercury, seen in a very new light, continues to give up its secrets.&#8221;</p>
<p><strong>Farewell Spirit; New Science from Opportunity:</strong></p>
<p>Few could argue the success and the legacy of the twin Mars Exploration Rovers Spirit and Opportunity.  From their launch in June and July 2003, respectively, and their arrival on the red planet on 4 January 2004 and 25 January 2004, respectively, the twin rovers have beyond exceeded all expectations for their scientific mission which was only supposed to last 90 solar days.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z9.jpg"><img class="alignleft size-full wp-image-22422" title="Z9" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z9.jpg" alt="" width="351" height="275" /></a>For Opportunity, the journey on the red planet continues to this day with ongoing scientific evaluations into the past habitability of Mars and the planet&#8217;s current environmental conditions.</p>
<p>But for Opportunity&#8217;s twin rover Spirit, the rover which was launched first and arrived first on the red planet, the incredible journey came to a formal conclusion earlier this year when all attempts to communicate with the rover over the previous year proved unsuccessful.</p>
<p>After 2210 solar days on the surface of Mars, the final communication with the Spirit rover was received on 22 March 2010 at the beginning of what was expected to be a period of winter dormancy for the two rovers as they entered the Martian winter.</p>
<p>However, while Opportunity weathered the Martian winter, Spirit did not.  After 14 months of unsuccessful attempts to communicate with the rover, NASA officially ended Spirit&#8217;s tenure on Mars on 24 May 2011.</p>
<p>With an original mission duration of only 90 solar days, the Spirit rover functioned above and beyond what her engineers and scientists asked her to do. Functioning 24.5 times longer than anticipated, Spirit covered 4.8 miles during her 6 year 2 month 18 day tenure on Mars, nearly 12 times the original distance goals set for the mission.</p>
<p>According to NASA, &#8220;Our job was to wear these rovers out exploring, to leave no unutilized capability on the surface of Mars, and for Spirit we have done that.&#8221;</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z101.jpg"><img class="alignleft size-full wp-image-22423" title="Z10" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z101.jpg" alt="" width="350" height="261" /></a>Spirit was given a formal farewell on NASA television in the final week of May 2011, after which the assets that once belonged to Spirit and its mission were turned over to MSL mission team in preparation for that flight&#8217;s launch in November.</p>
<p>But with the demise of Spirit came a renewed focus on her twin, Opportunity.  Now the longest surviving vehicle on the surface of Mars, a title the Opportunity rover has held since April 2010, Opportunity is currently exploring the rim of Endeavour crater on Mars &#8211; a crater, like the Shuttle orbiter Endeavour, named after the 18th century British sailing vessel commanded by James Cook during his first voyage of discovery to Fiji, New Zealand, and Australia.</p>
<p>Over the course of the Opportunity&#8217;s nearly eight year tenure on the Martian surface, the rover has driven an impressive 21 miles and has functioned more than 30 times longer than its originally planned 90 solar day mission.</p>
<p>To this day, Opportunity continues to perform extensive geological analysis of Martian rocks and planetary surface features, including the very recent discovery of a mineral vein deposited by water on the surface of Mars.</p>
<p>In October of this year, Opportunity and her twin, Spirit, were selected for lifetime achievement award honors as part of the Breakthrough Awards presented by Popular Mechanics magazine.</p>
<p><strong>Dawn in the asteroid belt - Achieving orbit of Vesta:</strong></p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z117.jpg"><img class="alignleft size-full wp-image-22424" title="Z11" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z117.jpg" alt="" width="330" height="370" /></a><a href="http://www.nasaspaceflight.com/2007/09/delta-ii-finally-launches-with-dawn/" target="_blank">Launched aboard a Delta II rocket on 27 September 2007</a>, the Dawn spacecraft completed its near four year journey to the asteroid belt on 16 July 2011 when it entered orbit of the Vesta asteroid.</p>
<p>After being captured by Vesta&#8217;s gravity, the Dawn spacecraft maneuvered itself into a lower and closer orbit by firing its xenon ion rocket engines to enter a 4.3-hour low altitude mapping orbit.</p>
<p>For the Dawn mission, the goal of the overall flight is to characterize the conditions and processes of the solar system&#8217;s earliest eon by investigating the two largest protoplanets, Ceres and Vesta.</p>
<p>Vesta, the second most massive asteroid in the asteroid belt after the dwarf planet Ceres, is estimated to contain approximately 9% of the total mass of the asteroid belt.</p>
<p>Comparatively, though, little is known about Vesta except that it is one of the largest protoplanetary objects remaining intact since the formation of the solar system.  Currently, it is believed that both Ceres and Vesta formed in two different regions of the early solar system before migrating to their current location within the asteroid belt.</p>
<p>Since its arrival in July, the Dawn spacecraft has helped shed new light on Vesta, including the fact that it appears to be one of the most rugged &#8211; in terms of surface topography &#8211; bodies in the asteroid belt.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z122.jpg"><img class="alignleft size-full wp-image-22425" title="Z12" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z122.jpg" alt="" width="348" height="230" /></a>While information on how the surface features of Vesta were formed is still forthcoming, Dawn has revealed that some of the surface features of the asteroid in its southern hemisphere are only 1-2 billion years old, considerably younger than regions on the asteroid&#8217;s northern hemisphere.</p>
<p>Dawn has also helped reveal an interesting diversity in the composition of the craters on Vesta as well as the asteroid&#8217;s overall surface composition.</p>
<p>In all, Dawn has roughly seven more months of observations at Vesta before its ion engines will be fired again to take it out of orbit of Vesta and put the spacecraft on course for rendezvous with the dwarf planet Ceres in February 2015.</p>
<p><strong>Cassini at Saturn - The storm on Saturn and the year of Saturnian moons:</strong></p>
<p>Perhaps one of the most interesting scientific missions to take place in 2011 was the ongoing mission of Cassini at Saturn.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z132.jpg"><img class="alignleft size-full wp-image-22426" title="Z13" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z132.jpg" alt="" width="351" height="265" /></a>From discovering new heat sources on Saturn&#8217;s intriguing moon Enceladus, <a href="http://www.nasaspaceflight.com/2005/09/cassini-spots-titan-shoreline/" target="_blank">to finding that seasonal rains transform the surface of Titan</a>, to observing a raging storm on Saturn itself, and finally to a flyby of Enceladus, the Cassini mission has given us invaluable insight into the Saturnian system.</p>
<p>Beginning the year with the incredible discovery that heat output from the south polar region of Saturn&#8217;s moon Enceladus was much greater than originally thought possible, NASA&#8217;s Cassini spacecraft showed that heat-generated power was approximately 15.8 gigawatts in Enceladus&#8217; southern polar region.</p>
<p>While Enceladus&#8217; geologically active southern polar region was discovered in 2005, a 2007 study, according to NASA, &#8220;predicted the internal heat of Enceladus, if principally generated by tidal forces arising from the orbital resonance between Enceladus and another moon, Dione, could be no greater than 1.1 gigawatts averaged over the long term&#8221; &#8211; a hypothesis proved incorrect about Cassini earlier this year.</p>
<p>A possible explanation for the high heat flow observed in Enceladus could have a great deal to do with the amount of liquid water present under Enceladus&#8217; surface.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z152.jpg"><img class="alignleft size-full wp-image-22428" title="Z15" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z152.jpg" alt="" width="349" height="247" /></a>This potential explanation for the higher-than-expected power output on Enceladus comes from the direct measure of ice crystals released from underneath the surface of Enceladus by surface geysers.</p>
<p>These ice crystals, as sampled by Cassini during a flyby of Enceladus, contained salt-rich particles that could potentially be frozen droplets of a saltwater ocean in contact with Enceladus&#8217; mineral-rich rocky core.</p>
<p>This potential discovery of a massive underground saltwater ocean on Enceladus, a liquid ocean made possible by tidal energy from Enceladus&#8217; interaction with other moons of Saturn and Saturn itself, has garnered a new astrobiological interest in Saturn&#8217;s moon as yet another place in the solar system where life could potentially exist.</p>
<p>Following on the heels of this discovery, the Cassini spacecraft observed methane rain showers around Titan&#8217;s equatorial regions.  Following observations of large rain cloud systems in 2010, a predominantly dark surface near Titan&#8217;s equatorial region indicates that Titan&#8217;s surface is directly affected by seasonal changes within the Saturnian system as well as weather systems on Titan itself.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z161.jpg"><img class="alignleft size-full wp-image-22429" title="Z16" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z161.jpg" alt="" width="347" height="266" /></a>According to a NASA news release on 17 March 2011, an arrow-shaped storm appeared in the equatorial regions on Sept. 27, 2010 and a broad band of clouds appeared the next month. Over the next few months, Cassini monitored short-lived surface changes of Titan&#8217;s surface.</p>
<p>These observations suggest that recent weather on Titan is similar to that over Earth&#8217;s tropics.</p>
<p>Furthermore, around the same time as these previous observations, Cassini also monitored the birth of a violent storm in Saturn&#8217;s northern hemisphere that eventually grew to stretch around the entire planet.</p>
<p>Initially witnessing the formation of the storm in December 2010, Cassini witnessed the rapid expansion of the storm that eventually produced a 3,000-mile-wide dark vortex.</p>
<p>The storm became the first major storm on Saturn to be observed by an orbiting spacecraft and studied at thermal and infrared wave lengths.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z141.jpg"><img class="alignleft size-full wp-image-22427" title="Z14" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z141.jpg" alt="" width="349" height="254" /></a>Since the storm&#8217;s creation, Cassini monitored the changing composition of Saturn&#8217;s atmosphere, including the appearance of ammonia from deep in the atmosphere, from a mixing of air from different levels.</p>
<p>Finally, in early November 2011, Cassini made a close flyby of Saturn&#8217;s moon Enceladus, acquiring the first detailed radar images of the moon on November 6.  The images were the first high resolution radar observations made of any icy moon other than Titan.</p>
<p>The flyby also provided scientists the opportunity to obtain detailed measurements of Enceladus&#8217; icy jets in order to make new measurements of hot spots underneath Enceladus&#8217; surface.</p>
<p><strong>To the edge of the solar system - Voyager 1 and the great unknown:</strong></p>
<p>For NASA&#8217;s unmanned interplanetary missions, 2011 ended with the exciting discovery that <a href="http://www.nasaspaceflight.com/2011/09/voyager-1s-great-escape-search-for-interstellar-space/" target="_blank">the Voyager 1 space probe is closer than thought to exiting the solar system and entering the interstellar medium</a>.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A20.jpg"><img class="alignleft size-full wp-image-22430" title="A20" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A20.jpg" alt="" width="351" height="266" /></a>Described by NASA has a cosmic purgatory, new information from the Voyager 1&#8242;s scientific instruments over the previous year indicate that the spacecraft has entered a new region between our solar system and interstellar space.</p>
<p>In this new region, the wind of charged particles streaming out from our sun, particles which compose the magnetic field of our solar system, begin to &#8220;pile up&#8221; while higher energy particles from inside our solar system appear to be leaking out into the interstellar medium.</p>
<p>According to NASA, &#8220;Voyager tells us now that we&#8217;re in a stagnation region in the outermost layer of the bubble around our solar system. Voyager is showing that what is outside is pushing back. We shouldn&#8217;t have long to wait to find out what the space between stars is really like.&#8221;</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A64.jpg"><img class="alignleft size-full wp-image-22431" title="A64" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A64.jpg" alt="" width="350" height="254" /></a>But while Voyager 1 is close to passing into the interstellar medium, indications from the spacecraft show that the magnetic field lines from the sun have not changed direction.  This is a direct indication that Voyager 1 is still within the heliosphere, the area in which the charged particles from the sun are still the dominant force.</p>
<p>While this new information is exciting and gives us a better understanding of the outer-most reaches of our solar system, it does not change the previous statement from NASA that Voyager 1 could enter the interstellar medium at any time now.</p>
<p>While the exact date on which Voyager 1 will exit the solar system, becoming the first manmade object to do so in recorded history, cannot be precisely calculated, all indications are that Voyager 1 will enter the interstellar medium sometime in the next few years.</p>
<p>Click here for our two previous Voyager Feature Articles:<br />
<a href="http://www.nasaspaceflight.com/2011/08/voyagers-unprecedented-on-going-mission-exploration/">http://www.nasaspaceflight.com/2011/08/voyagers-unprecedented-on-going-mission-exploration/</a><br />
<a href="http://www.nasaspaceflight.com/2011/08/thirty-four-years-voyager-2-continues-explore/">http://www.nasaspaceflight.com/2011/08/thirty-four-years-voyager-2-continues-explore/</a></p>
<p><strong>Into 2012 &#8211; A year to capitalize on what&#8217;s come before:</strong></p>
<p>While 2011 was a banner year for NASA in terms of interplanetary science, 2012 should be an even more exciting year. </p>
<p>In the next year, the MESSENGER spacecraft will continue its observations of planet Mercury while observing the planet at close range during the solar maximum cycle of our sun. It is hoped the MESSENGER will be able to monitor the solar maximum&#8217;s effect on the inner-most planet in our solar system.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A93.jpg"><img class="alignleft size-full wp-image-22432" title="A93" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/A93.jpg" alt="" width="352" height="329" /></a>Meanwhile, much closer to home, he twin GRAIL spacecraft will begin to unlock further secrets of our closest celestial neighbor in terms of its composition and formation in the early years of the solar system.</p>
<p>Furthermore, NASA will have the privilege of being the only space agency in the world to attempt a landing of a rover on Mars.  This distinction comes after the failed Martian launch attempt from Russia of the Fobos-Grunt probe in November 2011.</p>
<p>And while Cassini will continue to observe the Saturnian system and Voyager 1 continues to get ever-closer to the interstellar boundary between our solar system and interstellar space, NASA will conduct of the launch of the NuSTAR, the Nuclear Spectroscopic Telescope Array to allow astronomers to study the universe in high energy X-rays.</p>
<p>That mission is currently scheduled to launch on March 14, 2012 aboard the Pegasus XL rocket from the Reagan Test Site in Kwajalein Atoll.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z171.jpg"><img class="alignleft size-full wp-image-22433" title="Z17" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z171.jpg" alt="" width="351" height="250" /></a>This will be followed by the launch of the Radiation Belts Storm Probes atop an Atlas V rocket from the Cape Canaveral Air Force Station.</p>
<p>This mission, dubbed RBSP, will help our understanding of the sun&#8217;s influence on Earth and near-Earth space by studying the Earth&#8217;s radiation belts on various scales of space and time.</p>
<p>That mission is currently scheduled to launch on August 23, 2012.</p>
<p>Following the launch of that mission, NASA will align itself for the launch of the Interface Region Imaging Spectrograph, or IRIS.  This mission, which is progressing toward a target launch date of December 1, 2012 will be flown aboard the Pegasus XL rocket from Vandenberg Air Force Base in California.</p>
<p>The mission itself is designed to provide information on energy transport into the corona and solar wind and provide an archetype for all stellar atmospheres.</p>
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<p>Related posts:<ol><li><a href='http://www.nasaspaceflight.com/2011/09/live-ula-deltaii-launch-grail-spacecraft-to-moon/' rel='bookmark' title='Permanent Link: Delta II launches with moon-bound GRAIL spacecraft'>Delta II launches with moon-bound GRAIL spacecraft</a> <small>The Delta II rocket has launched on its 150th flight...</small></li>
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