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	<title>NASASpaceFlight.com &#187; Falcon</title>
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		<title>Stratolaunch introduce Rutan designed air-launched system for Falcon rockets</title>
		<link>http://www.nasaspaceflight.com/2011/12/stratolaunch-rutan-designed-air-launched-system-falcon-rockets/</link>
		<comments>http://www.nasaspaceflight.com/2011/12/stratolaunch-rutan-designed-air-launched-system-falcon-rockets/#comments</comments>
		<pubDate>Wed, 14 Dec 2011 03:05:58 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
				<category><![CDATA[Commercial]]></category>
		<category><![CDATA[Featured]]></category>
		<category><![CDATA[Falcon]]></category>
		<category><![CDATA[SpaceShipTwo]]></category>
		<category><![CDATA[SpaceX]]></category>
		<category><![CDATA[Stratolaunch]]></category>

		<guid isPermaLink="false">http://www.nasaspaceflight.com/?p=22222</guid>
		<description><![CDATA[Funded as a Paul G. Allen project under the banner of Stratolaunch, Burt Rutan is taking his space tourism concept a step further, by developing an air-launch system for payloads in the 10,000lbm class into Low Earth Orbit (LEO). The system will be able to launch from several possible operational sites and eventually aims to [...]


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</ol>]]></description>
			<content:encoded><![CDATA[<p>Funded as a Paul G. Allen project under the banner of Stratolaunch, Burt Rutan is taking his space tourism concept a step further, by developing an air-launch system for payloads in the 10,000lbm class into Low Earth Orbit (LEO). The system will be able to launch from several possible operational sites and eventually aims to provide crewed services.</p>
<p><span id="more-22222"></span><strong>Stratolaunch:</strong></p>
<p>The air-launch system is made up of four primary elements: a carrier aircraft &#8211; <a href="http://www.nasaspaceflight.com/2006/09/virgin-galactic-reveals-vss-enterprise/" target="_blank">a super large derivative of SpaceShipTwo&#8217;s carrier plane</a>, a multi-stage booster &#8211; namely a Falcon 4 or 5, a mating and integration system, and an orbital payload.</p>
<p>Very few actual details were revealed at the Seattle media event, partly due to competition issues and partly because the concept has not yet reached the Preliminary Design Review (PDR) stage and thus only exists on hundreds of technical drawings.</p>
<div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?board=6.0">Commercial 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>However, Stratolaunch confirmed that their initial efforts will focus on unmanned payloads, citing a gap in the market for the Delta II class upmass league &#8211; as much as they omitted mentioning other vehicles they will be in competition with, such as the recently renamed Antares, which will be operated by Orbital.</p>
<p>&#8220;Stratolaunch Systems has assembled a team of innovative aerospace leaders to build and deliver a commercial air launch system. Scaled Composites will build the carrier aircraft; SpaceX will provide the booster and space launch mission design and mission integration services,&#8221; noted the company&#8217;s release on Tuesday.</p>
<p>&#8220;Dynetics will provide program management and systems engineering and integration, as well as test and operations support to Stratolaunch; Dynetics will also build the mating and integration system hardware. Stratolaunch Systems headquarters are in Huntsville, Alabama, and its aircraft hangar is in Mojave, California.&#8221;</p>
<p>The concept of air-launch is nothing new, leading to somewhat of a mixed reaction in parts of the space flight community. Orbital themselves operate a <a href="http://www.nasaspaceflight.com/2008/10/ibex-orbital-pegasus-live/" target="_blank">smaller scale air-launch system via their Pegasus rocket</a> &#8211; which is launched from underneath their L-1011 aircraft.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z26.jpg"><img class="alignleft size-full wp-image-22228" title="Z2" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z26.jpg" alt="" width="349" height="221" /></a>Other concepts &#8211; such as the ALTO Crossbow System &#8211; have been seen over the years, with the aforementioned system based on an airframe which could launch various rockets and transporters.</p>
<p><a href="http://forum.nasaspaceflight.com/index.php?topic=2011.0" target="_blank">Conceptual designs and graphics (L2)</a> show this system with a Delta IV rocket being carried by the airframe, which is roughly what Stratolaunch are proposing with their design.</p>
<p>Stratolaunch&#8217;s carrier aircraft, built by Scaled Composites, weighs more than 1.2 million pounds and has a wingspan of 385 feet. Using six 747 engines, the carrier aircraft will be the largest aircraft ever constructed.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z34.jpg"><img class="alignleft size-full wp-image-22229" title="Z3" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z34.jpg" alt="" width="353" height="187" /></a>The air-launch system requires a takeoff and landing runway that is, at minimum, 12,000 feet long. The carrier aircraft can fly over 1,300 nautical miles to reach an optimal launch point.</p>
<p>The company announced they have already acquired two 747s to become the opening hardware for this system.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z43.jpg"><img class="alignleft size-full wp-image-22230" title="Z4" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z43.jpg" alt="" width="353" height="197" /></a><a href="http://www.nasaspaceflight.com/tag/spacex/" target="_blank">The multi-stage booster is derived from SpaceX&#8217;s Falcon 9 rocket</a>, with Tuesday&#8217;s media event noting this vehicle will be either a Falcon 4 or Falcon 5 vehicle &#8211; based on the number of engines it will use.</p>
<p>&#8220;Paul Allen and Burt Rutan helped generate enormous interest in space with White Knight and SpaceShipOne,&#8221; said SpaceX President Gwynne Shotwell. &#8220;There was no way we weren&#8217;t going to be involved in their next great endeavor. We are very excited.&#8221;</p>
<p>At approximately 120 feet long, the booster is designed to loft the payload into LEO. After release of the booster from the aircraft at approximately 30,000 feet, the first stage engines ignite and the spacecraft begins its journey into space.</p>
<p>After the first stage burn and a short coast period, the second stage ignites and the orbital payload proceeds to its planned mission. The booster&#8217;s health and status during flight is monitored from the carrier aircraft and on the ground.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z52.jpg"><img class="alignleft size-full wp-image-22231" title="Z5" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z52.jpg" alt="" width="352" height="218" /></a>Although the carrier plane&#8217;s role will be based heavily on Burt Rutan&#8217;s heritage at Scales Composites, the challenge of being able to host such a large launch vehicle safely will be partly down to Dynetics to solve, as their work on the mating and integration system (MIS) aims to provide the single interface between the carrier aircraft and the booster.</p>
<p>&#8220;We are excited to play such a major role on this system. This is an ambitious project unlike any that has been undertaken and I am confident the Stratolaunch team has the experience and capabilities to accomplish the mission,&#8221; said Dynetics Executive Vice President and Stratolaunch Board Member David King.</p>
<p>The MIS includes all systems required for the booster to interface with the carrier aircraft, including mechanical, electrical, thermal, fluids, and gases. The MIS is designed to safely and securely carry a booster weighing up to roughly 500,000 pounds.</p>
<p>The MIS will secure the booster to the carrier aircraft, from taxiing to flight maneuvers to release of booster.  In the case of a mission abort, the MIS will keep the booster secure during return to base and landing.</p>
<p>The mating and integration system will be manufactured in Huntsville, Alabama in Dynetics&#8217; new 226,500 square foot prototyping facility.</p>
<p><a href="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z61.jpg"><img class="alignleft size-full wp-image-22232" title="Z6" src="http://www.nasaspaceflight.com/wp-content/uploads/2011/12/Z61.jpg" alt="" width="342" height="329" /></a>Investor and philanthropist Paul G. Allen is the man with the money behind the project, with all other related companies acting as subcontractors to Stratolaunch. Mr Allen co-founded Microsoft with Bill Gates in 1975 and remained the company&#8217;s chief technologist until he left Microsoft in 1983. He is the founder and chairman of Vulcan Inc. which oversees his business and philanthropic efforts.</p>
<p>In 2004, <a href="http://www.nasaspaceflight.com/?s=SpaceShipOne" target="_blank">Allen funded SpaceShipOne, the first privately-backed effort to successfully put a civilian in suborbital space</a> and winner of the Ansari X-Prize competition. Stratolaunch&#8217;s drive is a direct follow on from Allen and Rutan&#8217;s original partnership.</p>
<p>&#8220;I have long dreamed about taking the next big step in private space flight after the success of SpaceShipOne &#8211; to offer a flexible, orbital space delivery system,&#8221; Allen said. &#8220;We are at the dawn of radical change in the space launch industry. Stratolaunch Systems is pioneering an innovative solution that will revolutionize space travel.&#8221;</p>
<p>The Stratolaunch system will eventually have the capability of launching people into low earth orbit. But the company is taking a building block approach in development of the launch aircraft and booster, with initial efforts focused on unmanned payloads. Human flights will follow, after safety, reliability and operability are demonstrated.</p>
<p>Mr Allen himself admitted that he would not want to fly in either SpaceShipTwo or this new concept until it had proven itself many times over. He cited being conservative about life as the main reason for being wary.</p>
<p>(Images via Stratolaunch and L2)</p>
<img src="http://www.nasaspaceflight.com/wp-content/plugins/pixelstats/trackingpixel.php?post_id=22222&amp;ts=1328833417" style="display:none;" alt="pixelstats trackingpixel"/>

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</ol></p>]]></content:encoded>
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		<title>Ares/Orion slipping up to 18 months &#8211; Shuttle extension gains upper hand</title>
		<link>http://www.nasaspaceflight.com/2009/03/aresorion-slipping-18-months-shuttle-extension-upper-hand/</link>
		<comments>http://www.nasaspaceflight.com/2009/03/aresorion-slipping-18-months-shuttle-extension-upper-hand/#comments</comments>
		<pubDate>Fri, 27 Mar 2009 17:34:08 +0000</pubDate>
		<dc:creator>Chris Bergin</dc:creator>
				<category><![CDATA[Featured]]></category>
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		<guid isPermaLink="false">http://www.nasaspaceflight.com/?p=9332</guid>
		<description><![CDATA[NASA&#8217;s Constellation Program (CxP) will conduct a &#8220;Content and Schedule&#8221; summit meeting in the next few months, after it was evaluated their current schedules are &#8220;broken&#8221;. The meeting will aim to protect against a slip that is estimated to be as serious as 18 months, or outright cancellation for Ares I. Meanwhile, the push for [...]


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</ol>]]></description>
			<content:encoded><![CDATA[<p>NASA&#8217;s Constellation Program (CxP) will conduct a &#8220;Content and Schedule&#8221; summit meeting in the next few months, after it was evaluated their current schedules are &#8220;broken&#8221;. The meeting will aim to protect against a slip that is estimated to be as serious as 18 months, or outright cancellation for Ares I. Meanwhile, the push for extending the shuttle program by at least two years is gaining serious momentum.</p>
<p><span id="more-9332"></span></p>
<p><strong>Constellation Turmoil:<br />
</strong></p>
<p>Constellation&#8217;s schedules have been slipping at an alarming rate over the past few years, <a href="http://www.nasaspaceflight.com/2008/08/constellation-confirm-ioc-slip-to-orion-schedule/" target="_blank">with the last PMR (Program Milestone Review) confirming a 12 month slip in the IOC (Initial Operational Capability) to March, 2015</a>. This date relates to Orion 2, with Orion 4 &#8211; currently classed as the first crew rotation for the International Space Station (ISS), otherwise known as FOC (Full Operational Capability) &#8211; launching one year later in March, 2016.</p>
<p>While these dates continue to be the official timeline, internal reviews have found those schedules to be &#8220;broken&#8221;, with CxP departments across the program reporting they are at &#8220;zero percent confidence&#8221; for keeping to the March, 2015 (IOC) timeline.</p>
<div>
<p>The problem isn&#8217;t just funding &#8211; which has become problematic for CxP over the last few years &#8211; but also what is described as &#8220;serious disconnects&#8221; between related departments, such as Orion, Ground Ops and Ares.</p></div>
<p>While continued changes to the designs of Ares and Orion are part of the natural development cycle, <a href="http://www.nasaspaceflight.com/2008/12/ares-i-thrust-oscillation-meetings-encouraging-allowance-for-changes/" target="_blank">issues such as Thrust Oscillation</a> and vehicle performance have come at a price for both schedule and costings, despite <a href="http://www.nasaspaceflight.com/2008/12/ares-i-thrust-oscillation-meetings-encouraging-allowance-for-changes/" target="_blank">fine work from the engineering teams tasked with mitigating</a> the issues.</p>
<p><img class="alignleft size-full wp-image-9336" title="a314" src="http://www.nasaspaceflight.com/wp-content/uploads/2009/03/a314.jpg" alt="a314" width="150" height="267" />CxP attempted to protect the schedule and budgetary pressures by offsetting these additional strains by <a href="http://www.nasaspaceflight.com/2008/10/constellation-deleting-ares-test/" target="_blank">deleting test items &#8211; notably on the Upper Stage</a>. However, this only proved to cause further disconnects throughout the program.</p>
<p>Issues with the <a href="http://www.nasaspaceflight.com/2008/05/ares-progress-update-opening-j-2x-engine-tests-completed/" target="_blank">Ares I Upper Stage engine, J-2X</a>, have also been noted, although no specific information has been made available due to the classified nature of certain vehicle elements.</p>
<p>&#8220;Disconnects&#8221; have been previously noted on various stages of the vehicle, such as with a key Launch Abort System (LAS) test, cancelled with just 24 hours notice due to additional testing requirements being cited by the Orion program, adding months to the realigned test schedule, which in turn added further strain to <a href="http://www.nasaspaceflight.com/2008/09/orion-pdr-delay-could-stretch-into-2010/" target="_blank">the already heavily-delayed Orion PDR (Preliminary Design Review)</a>.</p>
<p>Orion contractor Lockheed Martin were already <a href="http://www.nasaspaceflight.com/2008/09/orions-plea-to-ares-i-stop-adversely-hindering-our-design-process/" target="_blank">complaining last year about continued changes to the requirements of vehicle</a>, which is likely to undergo another major change during the upcoming summit meeting, after it was noted <a href="http://www.nasaspaceflight.com/2009/03/orion-opts-for-hybrid-lite-comms-system/" target="_blank">the switch from a crew of six to four </a>will be a lead item for discussion.</p>
<p>Several vehicle systems have been progressing through their development cycle to plan, but have subsequently suffered via waiting for related systems to catch up due to technical challenges, or return to a steady funding cycle, in turn causing a schedule mismatch &#8220;ripple effect&#8221; through the master timeline.</p>
<p>The summit will attempt to realign all the individual schedules, find potential funding &#8216;get-wells&#8217;, and create a viable timeline to try and bring Ares and Orion back into the March 2015 IOC target. However, confidence this can be achieved without a major boost to Constellation funding is classed as low.</p>
<p><strong>Gap Reduction:</strong></p>
<p>The serious nature of the &#8220;broken&#8221; schedules have been known for a few months, with an immediate slip of six months added internally to the master schedule, during a period when <a href="http://www.nasaspaceflight.com/2008/10/constellation-deleting-ares-test/" target="_blank">CxP were evaluating acceleration options</a>. This occurred prior to the latest estimate of a slip of between 12 to 18 months &#8211; in total &#8211; on top of the current schedule.</p>
<div><span style="MS Shell Dlg;"><span style="Arial;"><div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php?action=collapse;c=3;sa=collapse;#3">Constellation Forum Sections</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?board=29.0">L2 Ares/Orion Sections (over several hundred gbs in size)</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div></span></span></div>
<p>Those acceleration options have since fallen by the wayside, with the worst case cost estimate coming in at around $7 billion just to bring the program back to the 2007 tatget of a 2014 launch of Orion 2. The priority now is to attempt to find a &#8220;magic solution&#8221; of bringing Ares/Orion in with a shot of making the March, 2015 IOC date. Avoiding further slips to the right is the goal, as opposed to acceleration of the schedule.</p>
<p>The situation with Ares is known in key areas of the Agency, with a &#8220;9th Floor&#8221; NASA HQ effort already taking place to evaluate the viability of cancelling Ares I, and replacing the launch vehicle with an EELV (Evolved Expendable Launch Vehicle) &#8211; such as an Atlas V Heavy or a Delta IV Heavy &#8211; <a href="http://www.nasaspaceflight.com/2008/12/ssme-ares-v-undergoes-evaluation-potential-switch/" target="_blank">whilst moving the Marshall Space Flight Center (MSFC) effort towards concentrating on Ares V</a>.</p>
<p>NASA managers <a href="http://www.nasaspaceflight.com/2008/09/senate-pass-nasa-bill-for-extra-funding/" target="_blank">have alternative options, including COTS-D</a>, which would initiate SpaceX into bringing their <a href="http://www.nasaspaceflight.com/2009/01/musk-ambition-spacex-aim-for-fully-reusable-falcon-9/" target="_blank">Dragon manned vehicle on line</a> as a bufferzone during the gap. However, while NASA are supportive of SpaceX&#8217;s efforts, sources claim it would take a major leap of faith to hand the task of buffering the gap to such a &#8216;new&#8217; space flight company.</p>
<p><strong>Shuttle Extension:</strong></p>
<p><a href="http://www.nasaspaceflight.com/2008/09/nasas-dream-scenario-of-a-13-flight-extension-for-shuttle/" target="_blank">Building up a head of steam is shuttle extension, with wide-scale support at both the program and political level</a>. Initially curtailed by former NASA administrator Mike Griffin &#8211; who was firmly in the Ares camp &#8211; the strongest wording in favour of extension, at a program level, was seen this week on the Shuttle Stand-Up/Integration report, on L2.</p>
<div><span style="MS Shell Dlg;"><span style="Arial;"><div class="L2Info right"><h4>See Also</h4><ul><li><a href="http://forum.nasaspaceflight.com/index.php#2">Downstream Mission UPDATES</a></li><li><a href="http://forum.nasaspaceflight.com/index.php?action=tags&amp;tags=2015">L2 Extension Docs and Memos</a></li><li><a href="http://www.nasaspaceflight.com/l2/">Click here to Join L2</a></li></ul></div></span></span></div>
<p>&#8220;Last week, around 200 prime contractors and suppliers went to Washington D.C. and got briefs from the Hill and key NASA people,&#8221; noted the report. &#8220;They went over to the Hill and talked to over 100 Congress representatives or their staffers.</p>
<p>&#8220;The message was that the Shuttle is operating well and is safe to fly.&#8221;</p>
<p>That &#8220;message&#8221; directly counters Mr Griffin&#8217;s efforts to warn against extending the shuttle, after citing safety numbers that intimated a disaster was on the cards if the vehicles flew past 2010. It also makes the point the shuttle is an operating vehicle, whereas the alternatives remain out of sight.</p>
<p>The report goes on to note the need to avoid CxP from falling yet further behind its originally schedule &#8211; whereas previous statements have alluded to the possibility of acceleration &#8211; which is no longer viable without additional billions being pumped into the program, potentially the same amount it would take to extend the shuttle by two years.</p>
<p>&#8220;To close the gap it would be necessary to hold the funding to make sure the CxP does not move any further to the right, and to add additional funding if Congress deems it necessary to fly into 2011 and 2012,&#8221; added the report. &#8220;It was well received but these are tough budget times.&#8221;</p>
<p>There are conflicting numbers on how much it would cost to extend the shuttle program, with various options available. <a href="http://www.nasaspaceflight.com/2008/10/shuttle-extension-white-paper/" target="_blank">Most of the options opt for two orbiters flying though the extension, with one grounded as a &#8216;near flight ready&#8217; orbiter that can supply spares to her two sisters</a>.</p>
<p><img class="alignleft size-full wp-image-9335" title="a224" src="http://www.nasaspaceflight.com/wp-content/uploads/2009/03/a224.jpg" alt="a224" width="329" height="250" />Program milestone charts acquired just this week by L2 confirm that the <a href="http://www.nasaspaceflight.com/2009/02/shuttle-planning-clfs-ams-noted-maf-extra-ets/" target="_blank">Michoud Assembly Facility (MAF) &#8216;additional&#8217; tanks have been set up the purpose of pre-empting extension</a>, with opening work completed on at least two brand new tanks past the yet-to-be-approved STS-134.</p>
<p>A refurbished ET-122 is also available for STS-135 &#8211; currently the Launch On Need (LON) tank for STS-134.</p>
<p>Should extension receive the required funding, MAF would be able to build new tanks, as all the shuttle related tooling <a href="http://www.nasaspaceflight.com/2008/09/senate-pass-nasa-bill-for-extra-funding/" target="_blank">has been protected via the outlines in the recent Senate Bill</a>. However, a decision will need to be made soon, with layoffs of key skill set workers already taking place in New Orleans, and a systematic shutdown of shuttle related contractors soon to head past the point of no return.</p>
<p>The end of April has been deemed as D-Day for the shuttle program&#8217;s potential to extend. However, the in-built protection from the Senate Bill is understood to have gained enough time for the cut-off to be as late as the summer.</p>
<p>A lot will depend on what the next NASA administrator prefers, and more so the political will to find the best solution to ensure the United States does not suffer from a lack of domestic manned launch capability for over half a decade.</p>
<p><a href="http://www.nasaspaceflight.com/l2/"><em><span><span><span><em><span><span lang="EN-GB"><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span><span style="color: #0066cc;">L2 members</span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></span></em></span></span></span></em></a><em><span><span><em><span><span lang="EN-GB">: Documentation &#8211; from which the above article has quoted snippets &#8211; is available in full in the related L2 sections, now over 4000 gbs in size.</span></span></em></span></span></em></p>
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<p>Related posts:<ol><li><a href='http://www.nasaspaceflight.com/2008/09/orion-pdr-delay-could-stretch-into-2010/' rel='bookmark' title='Permanent Link: Orion PDR delay could stretch into 2010'>Orion PDR delay could stretch into 2010</a> <small>The requirement to carry out an additional Design Analysis Cycle...</small></li>
<li><a href='http://www.nasaspaceflight.com/2007/07/orion-weight-saving-refinements-continue-focus-on-iss-access/' rel='bookmark' title='Permanent Link: Orion weight saving refinements continue &#8211; focus on ISS access'>Orion weight saving refinements continue &#8211; focus on ISS access</a> <small>The Lockheed Martin Orion spacecraft has received a new set...</small></li>
<li><a href='http://www.nasaspaceflight.com/2007/10/saving-spaceship-orion-zero-base-vehicle-task-complete/' rel='bookmark' title='Permanent Link: Saving spaceship Orion &#8211; Zero Base Vehicle task complete'>Saving spaceship Orion &#8211; Zero Base Vehicle task complete</a> <small>NASA Constellation and Lockheed Martin engineers have completed the first...</small></li>
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