Orbital Sciences X-34
From Spacefaring
Q547844
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.
1999
Wikimedia, Wikidata
X-34
length 17.77 metre, height 3.5 metre, mass 21770 kilogram, mass 8165 kilogram,
Orbital Sciences Corporation, National Aeronautics and Space Administration, United States,
NASA, United States, Dong Fang Hong 2, sub-orbital spaceplane, 1999, 1990s,
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Location: KML, Cluster Map, Maps,
1999-06-29T00:00:00Z
1999-06-29T00:00:00Z
1999 Orbital Sciences X-34
1999-06-29T00:00:00Z
1999-06-29T00:00:00Z
maiden flight
2001-03-31T00:00:00Z
2001-03-31T00:00:00Z
project cancellation
1996-08-28T00:00:00Z
1996-08-28T00:00:00Z
construction contract
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| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | X-34 wind tunnel | Commons | ||
| commons | image | X-34 wind tunnel | Commons | ||
| commons | image | This is the X-34 Technology Testbed Demonstrator being mated with the L-1011 mothership. The X-34 will demonstrate key vehicle and operational technologies applicable to future low-cost resuable launch vehicles. | Commons | ||
| commons | image | Orbital Sciences X-34 | Commons | ||
| commons | image | X-34 at NASA Dryden Flight Research Center - GPN-2000-000185 | Commons | ||
| commons | image | X-34 Technology Testbed Demonstrator on NASA Dryden ramp | Commons | ||
| commons | image | Orbital Sciences X-34 | Commons | ||
| commons | image | X-34 mated to modified L-1011 during takeoff on first captive carry flight | Commons | ||
| commons | image | X-34 mated to modified L-1011 during takeoff on first captive carry flight | Commons | ||
| commons | image | X-34 mated to modified L-1011 during takeoff on first captive carry flight | Commons | ||







