Antares lofts ORB-2 Cygnus on a path to the ISS

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Orbital Sciences launched an Antares rocket with their third Cygnus spacecraft Sunday afternoon, beginning a commercial resupply mission to the International Space Station. The rocket launched at the end of a very smooth countdown at 12:52 local time (16:52 UTC) from Pad 0A at the Mid-Atlantic Regional Spaceport.


Antares Launch with ORB-2 Cygnus:

Cygnus was developed by Orbital Sciences Corporation under NASA’s Commercial Orbital Transportation Services (COTS) program, under which it made its first flight last September.

Following this successful demonstration mission Orbital began fulfilling the launches they were awarded under a Commercial Resupply Services contract signed in 2008.

Z54Cygnus was not originally the first choice for the COTS program; Rocketplane Kistler’s reusable K-1 vehicle had originally been selected, along with SpaceX’s Dragon, for development.

The K-1 fell behind schedule and Kistler’s contract was terminated in late 2007, with Orbital being awarded the replacement contract in February 2008.

SpaceX’s development of the Dragon was unaffected, and that spacecraft has conducted five successful missions to date.

Unlike Dragon, which has the ability to return cargo to Earth, the Cygnus is designed solely to deliver cargo to the International Space Station – burning up in the atmosphere at the end of its mission like Russia’s Progress, Europe’s ATV or Japan’s Kounotori.

2014-07-13 13_42_52-antares and cygnus - Google SearchBuilding upon technology developed for Orbital’s Star series of geosynchronous communications satellites, the Cygnus incorporates a Pressurized Cargo Module (PCM) developed by Thales Alenia Space and based upon the design of Multi-Purpose Logistics Modules (MPLMs) carried by the Space Shuttle.

A Cygnus variant with an unpressurised cargo section, based on another Shuttle payload – the ExPRESS Logistics Carrier – was also proposed, but this was not developed.

The Cygnus spacecraft is powered by an IHI Aerospace Delta-V engine, a derivative of the BT-4 engine, which is typically used by communications satellites.

The engine can operate in monopropellant or bipropellant modes utilising hydrazine fuel. In bipropellant mode, mixed oxides of nitrogen (MON-3) are used to oxidise the propellant.

2014-07-13 13_48_18-index.php (2832×4256)The main engine produces 445 newtons (100 pounds) of thrust, while thirty two smaller reaction control thrusters, used for manoeuvring and orientation, each provide 27 newtons (6 pounds) of thrust.

The Pressurized Cargo Module can accommodate 2,000 kilograms (4,410 lb) of cargo and has a volume of 18.2 cubic metres (643 cubic feet). Power is provided by a pair of triple-junction gallium arsenide solar arrays which generate 3.5 kilowatts.

The forward end of the spacecraft is equipped with a Common Berthing Mechanism (CBM) which allows attachment to the International Space Station upon arrival.

Z3ARather than docking under its own control and power, Cygnus missions manoeuvre close to the ISS before being captured by the station’s robotic arm, Canadarm2, and transferred to a node – usually Harmony – for berthing.

Sunday’s mission, CRS Orb-2, has also been named the SS Janice E. Voss, after the NASA astronaut who died of cancer in 2012, following Orbital’s tradition of naming its Cygnus craft after astronauts.

The spacecraft is carrying 1,494 kilograms (3,293 lb) of cargo, which NASA have divided into five categories. The largest, crew supplies, consists of food and other provisions as well as clothes or hygiene equipment for the astronauts.

The mass of this type of cargo being carried is 764 kilograms (1,684 lb). The payload also includes 355 kilograms (783 lb) of station hardware, including parts for the life support system, medical equipment, electrical and thermal control parts amongst others.

Around 8 kilograms of computer and photography equipment, and 39 kg (87 lb) of EVA hardware are also aboard.

The remainder of the cargo consists of scientific equipment and a cluster of CubeSats to be deployed from the Kibo module later this year. The other experiments include an experiment called Dynamic Surf for the Japanese Space Exploration Agency, which is aimed at studying Marangoni convection, a heat transfer process between liquids and gasses.

NASA are flying fifteen Student Spaceflight Experiment Program (SSEP) investigations aboard the mission, which will make use of resources aboard the space station to conduct research as part of an outreach program.

2014-07-13 13_52_36-TechEdSat-4 - Google SearchThe TechEdSat-4 CubeSat, which will be deployed from Kibo, is one of twenty nine small satellites being carried for deployment from the station.

Designed for a ten-day mission it will be operated by the San Jose State University in collaboration with NASA and the University of Idaho. It follows on from the TechEdSat-3p spacecraft, which was deployed from the ISS last year having been delivered by the fourth Japanese Kounotori resupply mission.

The satellite’s mission is to demonstrate the use of a passive deorbiting system; deploying a sail behind the satellite to increase drag. It follows the three-unit form factor, with dimensions of 10 by 10 by 30 centimetres (4 x 4 x 12 in).

2014-07-13 13_53_51-Flock-1b satellites - Google SearchThe other twenty eight satellites are all part of Planet Labs’ Flock constellation.

These Flock-1b satellites are identical to the Flock-1a spacecraft carried by the previous Cygnus mission in January and the eleven Flock-1c vehicles carried by a Dnepr launch last month.

Each spacecraft is a three-unit CubeSat equipped with an imaging system to produce images of the Earth for commercial use.

By operating a large fleet of satellites Planet Labs aims to be able to provide the most up-to-date imagery available.

Z6Sunday’s mission was carried by an Antares rocket. Originally named Taurus II, the Antares is a two-stage vehicle with a liquid-fuelled first stage and a solid-fuelled second stage.

This Antares will flew in the 120 configuration, which made its last flight. Consisting of the standard, AJ26-62 powered, first stage with an ATK Castor-30B second stage, the Antares carried its payload into Low Earth orbit.

The AJ-26 hardware on this flight had already been cleared for flight, following a test failure on a future engine at NASA Stennis.

Future missions will use the Antares 130 configuration, which replaces the Castor 30B with the ATK Castor 30XL, increasing the vehicle’s performance and thus its payload capacity.

This change will enable an enhanced version of the Cygnus spacecraft to begin flying next year.

Z38-350x225The first stage has two AJ26 engines, which are derivatives of the Soviet NK-33 which was developed for the N1 rocket in the late 1960s or early 1970s. The NK-33 is also used as the first stage engine of Russia’s Soyuz-2-1v.

The stage structure itself was developed by Ukraine’s Yuzhnoye Design Bureau, and is based on the first stage of the Zenit rocket.

Continuing to leverage existing hardware, the second stage of the Antares, the Castor-30, was developed from the Castor-120 used as the first stage of the Taurus (since renamed Minotaur-C) rocket.

This stage, which has also been used on Lockheed Martin’s Athena rocket, was itself a new-build version of the Peacekeeper missile’s first stage, to allow Peacekeeper-derived rockets to be used for commercial missions.

Z31Antares launches take place from Pad 0A at the Mid-Atlantic Regional Spaceport on Wallops Island.

The CRS-2 mission marked the fifth launch from the pad, which was first used in 1995 for the launch of an experimental satellite called METEOR atop a Conestoga 1620 rocket which failed to achieve orbit.

After failing on its maiden flight, the Conestoga was abandoned and Pad 0A fell into disuse. The original tower was demolished in 2008 to make way for the clean pad approach used by Orbital for the Antares, which first flew from the complex in April 2013. The three Antares launches from the pad prior to Sunday’s have all been successful.

The team that conducted Sunday’s launch were called to stations three hours and fifty minutes ahead of the planned liftoff. About three quarters of an hour later they conducted a poll for chilldown of the oxidiser lines which began ahead of oxidiser loading.

2014-07-13 13_50_21-Antares on launch pad - Google SearchPropellant loading began following another poll at the ninety minute mark in the count.

Fifteen minutes before liftoff, Cygnus was placed on internal power, with the Antares going on internal five minutes before it launched. The automated terminal count began at the three minutes before liftoff with the propellant tanks pressurising at around the 120-second mark.

When the count reached zero, the first stage engines ignited and began to build up thrust. After 2.1 seconds the rocket was released to begin her ascent towards orbit.

2014-07-13 13_51_08-8670674140_262b2ed869_z.jpg (640×427)Following liftoff the rocket climbed away from Wallops Island, passing through the area of maximum dynamic pressure around ninety seconds into the mission.

The first stage depleted its fuel supply around three minutes and fifty five seconds after launch, with the vehicle entering a coast phase while it ascended to an altitude of 202 kilometres (125 statute miles, 109 nautical miles).

Stage separation took place six seconds after cutoff, with the fairing separating 90 seconds later and the interstage five seconds after that. Four seconds after interstage separation the 105-second coast ended with second stage ignition.

2014-07-13 13_45_25-cygnus spacecraft engine - Google SearchThe solid-fuelled second stage is only capable of making one burn and cannot be shut down once started, so it burned to depletion.

This took 137 seconds, providing the final impulse needed to put Cygnus into orbit.

The planned parameters for spacecraft separation, which occurred two minutes after second stage burnout, were a perigee of 197 kilometres (122 miles, 106 nautical miles), an apogee of 303 kilometres (188 mi, 163 nmi), and 51.64 degrees inclination. It is understood they were well within the parameters following ascent.

Z3Following separation the spacecraft began its on-orbit checkout and deployed its solar arrays, before beginning a series of burns to reach the space station.

Arrival at the ISS is expected on the fourth day of the mission, with hatch opening the day after.

Cygnus is expected to remain at the Space Station for around thirty two days, during which time its cargo will be replaced with items for disposal. During its time at the station the spacecraft will be berthed at the nadir port of the Harmony module.

ATKFollowing unberthing, which will also be conducted using Canadarm2, the spacecraft will perform a series of flight tests for future missions before it is deorbited to a destructive reentry a few days later.

Sunday’s was the fortieth orbital launch attempt of 2014, the eleventh of the year for the United States, and the second for Orbital Sciences.

Orbital’s next launch is scheduled for October, and will be the next Cygnus mission, CRS Orb-3. That mission, which will mark the maiden flight of the Antares 130 and the last Cygnus mission before the introduction of an enhanced cargo module, is expected to be Orbital’s only remaining launch this year.

(Images: via L2′s Cygnus Section – Containing presentations, videos, a vast set of unreleased hi-res images, interactive high level updates and more, with additional images via Orbital and NASA).

(Click here: http://www.nasaspaceflight.com/l2/ - to view how you can support NSF and access the best space flight content on the entire internet).

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