Engineering:Pad Abort 1 (Orion)

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Pad Abort 1
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Launch of the Pad Abort 1 test
Mission typeAbort test
OperatorNASA
Mission duration95 seconds
Distance travelled2.1 kilometres (6,900 ft)
Apogee1.8 kilometres (6,000 ft)
Spacecraft properties
Spacecraft typeOrion boilerplate
Start of mission
Launch dateMay 6, 2010, 13:03:00 (2010-05-06UTC13:03Z) UTC
RocketOrion Launch Abort System
Launch siteWhite Sands LC-32E[1]
End of mission
Landing dateMay 6, 2010, 13:04:35 (2010-05-06UTC13:04:36Z) UTC
Orion Triangle Patch.svg  

Pad Abort 1 (PA-1) was a flight test of the Orion Launch Abort System (LAS). Orion was a component of Constellation, a human spaceflight project within NASA, the space agency of the United States. PA-1 was the first test in a sequence of atmospheric flight tests known as Orion Abort Flight Test (AFT).

PA-1 tested the basic functionality of the launch abort concept from the pad in its preliminary Orion design configuration. It used the former conformal shape of the LAS adapter. The Flight Test Article (FTA) vehicle will differ from production Orion vehicles in a number of ways. For example, the FTA will not have a crew on board, and the avionics will be a prototype of what is planned for production Orions.[2]

The PA-1 Test took place at the U.S. Army's White Sands Missile Range in New Mexico.

Gallery

References

 This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration.

External links

Orion Pad Abort 1 Video Highlights at Vimeohttp://vimeo.com/11631855