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Boeing X-40

From Wikipedia, the free encyclopedia
Test space vehicle
X-40
Boeing X-40A on a descent glide slope
General information
TypeGlide test vehicle
National originUnited States
ManufacturerBoeing Phantom Works
StatusRetired May 2001
Primary usersAir Force Research Laboratory
Number built1
History
First flightAugust 11, 1998
(dropped byUH-60 Black Hawk)[1][2][3]

TheBoeing X-40 Space Maneuver Vehicle is a test platform for theBoeing X-37 reusable spaceplane, built byBoeing Phantom Works. It sought to test the X-37's systems in order to "reduce the cost and risk of future reusable space launch vehicle system".[4]

History

[edit]

Theuncrewed X-40A was an 80%-90% subscale version of theBoeing X-37 reusable spaceplane, but lacking in propulsion or thermal protection systems. Boeing built the X-40A originally for the Air Force as part of that service’s Space Maneuver Vehicle program.[4][2]

The aircraft was built atBoeing Phantom Works atSeal Beach, California, in partnership with theAir Force Research Laboratory.[2]

After the firstdrop test in August 1998 the vehicle was transferred to NASA, which modified it. Between April 4 and May 19, 2001, the vehicle successfully conducted seven free flights.[2][3] In 2001 it successfully demonstrated theglide capabilities of the X-37's fat-bodied, short-winged design and validated the proposedguidance system.[citation needed]

Testing

[edit]

The first X-40A drop test occurred atHolloman AFB,New Mexico on August 11, 1998 at 06:59. It was released from an altitude of approximately 10,000 feet (3,000 m)[2] and 2.5 miles (4.0 km) away from the end of Runway 04 by aUH-60 Black Hawkhelicopter[1] (later tests used an ArmyCH-47D Chinook helicopter).[4][3] The vehicle dove to therunway in anapproach similar to theSpace Shuttle's, flared, and landed left of the runway centerline. Itsdrag chutes successfully deployed, and the vehicle tracked to within 7 feet (2.1 m) of the centerline and stopped at a distance of slightly more than 7,000 feet (2,100 m).

The X-40A flew seven approach and landing test flights at NASA’sDryden (now Armstrong) Flight Research Center inEdwards, California, in 2001 to reduce risk for the X-37 program, including in-flight evaluation of guidance, navigation and control software for its autonomous flight controls.[4] One test flight the craft was towed by an ArmyCH-47D Chinook helicopter to an altitude of 15,000 feet, and then released to fly an autonomously controlled 75-second descent to a landing on the main runway atEdwards Air Force Base, where it then glided and guided itself.[4]

Specifications (X-40A)

[edit]
X-40A on display at theNational Museum of the United States Air Force

Data fromBoeing X-40A - National Museum of the United States Air Force

General characteristics

  • Length: 22 ft (6.7 m)
  • Wingspan: 12 ft (3.7 m)
  • Empty weight: 2,600 lb (1,179 kg)

Performance

See also

[edit]

Related development

Related lists

References

[edit]

Public Domain This article incorporatespublic domain material from websites or documents of theNational Aeronautics and Space Administration.

  1. ^ab"Military Spaceplane X-40 Space Maneuver Vehicle Integrated Tech Testbed". Military Space Programs. Federation of American Scientists. Archived fromthe original on 11 March 2016.
  2. ^abcde"Boeing X-40A".National Museum of the United States Air Force. Retrieved2024-07-23.
  3. ^abcBoeing X-37 / X-40 page at Designation-Systems.Net
  4. ^abcdeGelzer, Christian (2 March 2016)."X-40A Space Maneuvering Vehicle".nasa.gov. Retrieved23 July 2024.

External links

[edit]
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