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The Orbital Sciences X-34 was intended to be a low-cost testbed for demonstrating "key technologies" that could be integrated into the Reusable Launch Vehicle program. It was intended to be an autonomous pilotless craft powered by a "Fastrac" liquid-propellant rocket engine, capable of reaching Mach 8 and performing 25 test flights per year.
Orbital Sciences Corporation (commonly referred to as Orbital) was an American company specializing in the design, manufacture, and launch of small- and medium- class space and launch vehicle systems for commercial, military and other government customers.
ANSI X3.4-1967, a character-encoding scheme Orbital Sciences X-34 , an American spaceplane program RFA Aldersdale (X34) , a fleet tanker of the Royal Fleet Auxiliary
The Taurus launch vehicle, later renamed [1] Minotaur-C (for "Minotaur-Commercial"), was the first of the Minotaur vehicle family, and the first ground-launched orbital booster developed by Orbital Sciences Corporation (OSC), derived by adding a solid booster stage to the air-launched Pegasus rocket. The first flight, sponsored by DARPA, was in ...
The goals of the program as of September 2013 were: [3] [17] The space plane must carry a 3,000–5,000 lb (1,400–2,300 kg) payload to low Earth orbit for less than a cost of US$5 million per flight, [4] at a rate of 10 or more flights per year; at that time, launching that type of payload requires using an Orbital Sciences Corporation Minotaur IV expendable booster, priced at $55 million ...
Orbital Sciences: 1: Retired 1997 [42] 2001 GEO STAR-2 (GEOStar-2) United States Orbital Sciences: 500 kg 3,325 kg 33 [43] Operational 2002 [42] 2013 GEO, 5550 W GEOStar-3: United States Orbital Sciences: 800 kg 5,000 kg 0: Development GEO, 8000 W SSTL-70 (Microsat-70) United Kingdom Surrey Satellite Technology: 30 kg 70 kg 16: Retired 1992 ...
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The Vega-C rocket's 4th stage payload dispenser AVUM acts as the service module for the shuttle, providing orbital manoeuvring and braking, power, and communications before being jettisoned for re-entry. [34] The AVUM service module replaces the integrated IXV Propulsion Module and frees 0.8 m 3 of internal space in the vehicle for a payload bay.
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