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|manufacturer = [[Boeing Phantom Works]]
|manufacturer = [[Boeing Phantom Works]]
|designer = <!--Only appropriate for single designers, not project leaders-->
|designer = <!--Only appropriate for single designers, not project leaders-->
|first flight = August 11 [[1998 in aviation|1998]]<br />(dropped by [[UH-60 Black Hawk]])<ref name="FAS.org">[http://fas.org/spp/military/program/launch/msp.htm X-40 Space Maneuver Vehicle Integrated Tech Testbed at FAS.org]</ref><ref name="GlobalSecurity.org">[http://www.globalsecurity.org/space/systems/x-40.htm X-40 Space Maneuver Vehicle (SMV) at GlobalSecurity.org]</ref><ref name="Designation-Systems.Net">[http://www.designation-systems.net/dusrm/app4/x-37.html Boeing X-37 / X-40 page at Designation-Systems.Net]</ref>
|first flight = August 11 [[1998 in aviation|1998]]<br />(dropped by [[UH-60 Black Hawk]])<ref name="FAS.org">[http://fas.org/spp/military/program/launch/msp.htm X-40 Space Maneuver Vehicle Integrated Tech Testbed at FAS.org]{{dead link}}</ref><ref name="GlobalSecurity.org">[http://www.globalsecurity.org/space/systems/x-40.htm X-40 Space Maneuver Vehicle (SMV) at GlobalSecurity.org]</ref><ref name="Designation-Systems.Net">[http://www.designation-systems.net/dusrm/app4/x-37.html Boeing X-37 / X-40 page at Designation-Systems.Net]</ref>
|introduction =
|introduction =
|status = Retired May 2001
|status = Retired May 2001
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* [http://www.nasa.gov/centers/dryden/multimedia/imagegallery/X-40A/index.html NASA Dryden X-40A Image Gallery]
* [http://www.nasa.gov/centers/dryden/multimedia/imagegallery/X-40A/index.html NASA Dryden X-40A Image Gallery]
* [https://web.archive.org/web/20060829082505/http://www.boeing.com:80/news/releases/1998/news_release_980811a.html X-40A Test Flight, Boeing press release]
* [https://web.archive.org/web/20060829082505/http://www.boeing.com:80/news/releases/1998/news_release_980811a.html X-40A Test Flight, Boeing press release]
* [http://fas.org/spp/military/program/launch/msp.htm X-40 Space Maneuver Vehicle Integrated Tech Testbed at FAS.org]
* [http://fas.org/spp/military/program/launch/msp.htm X-40 Space Maneuver Vehicle Integrated Tech Testbed at FAS.org]{{dead link}}
* [http://www.globalsecurity.org/space/systems/x-40.htm X-40 Space Maneuver Vehicle (SMV) at GlobalSecurity.org]
* [http://www.globalsecurity.org/space/systems/x-40.htm X-40 Space Maneuver Vehicle (SMV) at GlobalSecurity.org]
* [http://www.designation-systems.net/dusrm/app4/x-37.html Boeing X-37 / X-40 page at Designation-Systems.Net]
* [http://www.designation-systems.net/dusrm/app4/x-37.html Boeing X-37 / X-40 page at Designation-Systems.Net]

Revision as of 22:50, 8 May 2017

X-40A
Role Glide test vehicle
National origin United States
Manufacturer Boeing Phantom Works
First flight August 11 1998
(dropped by UH-60 Black Hawk)[1][2][3]
Status Retired May 2001
Primary users AFRL
NASA
Number built 1

The Boeing X-40A Space Maneuver Vehicle was a test platform for the X-37 Future-X Reusable Launch Vehicle.

History

The unpiloted X-40 was built to 85 percent scale to test aerodynamics and navigation of the X-37 Future-X Reusable Launch Vehicle project.

After the first drop 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.[3] In 2001 it successfully demonstrated the glide capabilities of the X-37's fat-bodied, short-winged design and validated the proposed guidance system.

Testing

The first X-40 drop test occurred at Holloman AFB, New Mexico on August 11, 1998 at 06:59. This was a joint Air Force/Boeing project known as Space Maneuver Vehicle. It was released from an altitude of approximately 9,200 feet (2,800 m) and 2.5 miles (4.0 km) away from the end of Runway 04 by a UH-60 Black Hawk helicopter[1][2][3] (later tests used the CH-47 Chinook helicopter).[2][3] The vehicle dove to the runway in an approach similar to the space shuttle's, flared, and landed left of the runway centerline. Its drag chutes successfully deployed, and the vehicle tracked to within seven feet of the centerline and stopped at a distance of slightly more than 7,000 feet (2,100 m).

Specifications (X-40)

General characteristics

  • Crew: None

Performance Avionics
Honeywell 12-channel Space Integrated GPS/INS (SIGI) system

See also

Related lists

References

External links