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Orbital Sciences X-34

Orbital Sciences X-34
Orbital Sciences X-34:Orbital Sciences X34
Description
RoleTechnology Testbed
CrewUnmanned
First FlightJune 29, 1999

(carried by a Lockheed L-1011)

ManufacturerOrbital Sciences Corporation, Dulles, VA
Dimensions
Length58 ft17.7 m
Wingspan28 ft8.5 m
Height12 ft3.7 m
Wing area358 ft²33.3 m²
Weights
Empty18,000 lb8,200 kg
Gross48,000 lb21,800 kg

The Orbital Sciences X-34 was intended as a low-cost testbed to demonstrate "key technologies" integratable to the Reusable Launch Vehicle program.

It was intended to be an autonomous pilotless craft powered by a Fastrac rocket engine capable of reaching Mach 8, and performing 25 test flights per year. However the unpowered prototype had only been used for towing and captive flight tests when the project was cancelled in 2001 on cost grounds. However, there is a possibility of using a scaled-up version of the X-34 as a hotel shuttle to a space hotel in the future. It would operate very similarly to the space shuttle; it will take off like a rocket, mated with two rocket boosters and an external fuel tank, dock with the space hotel like the shuttle does with the International Space Station, and land on a runway, the same way as an airplane. Even the overall design is very similar to 2001: A Space Odyssey 's Pan Am Orbital Clipper, the Orion III.


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Related development:

Comparable aircraft:

Designation Series: X-31 -X-32 -X-33 -X-34 -X-35 -X-36 -X-37

See also:


Categories


Spaceplanes | U.S. experimental aircraft 2000-2009

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