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The X-38 V-201 Fin Fold Actuation MechanismThe X-38 Vehicle 201 (V-201) is a space flight prototype lifting body vehicle that was designed to launch to orbit in the Space Shuttle orbiter payload bay. Although the project was cancelled in May 2003, many of the systems were nearly complete. This paper will describe the fin folding actuation mechanism flight subsystems and development units as well as lessons learned in the design, assembly, development testing, and qualification testing. The two vertical tail fins must be stowed (folded inboard) to allow the orbiter payload bay doors to close. The fin folding actuation mechanism is a remotely or extravehicular activity (EVA) actuated single fault tolerant system consisting of seven subsystems capable of repeatedly deploying or stowing the fins.
Document ID
20040084304
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Lupo, Christian
(NASA Johnson Space Center Houston, TX, United States)
Robertson, Brandan
(NASA Johnson Space Center Houston, TX, United States)
Gafka, George
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2004
Publication Information
Publication: 37th Aerospace Mechanisms Symposium
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-8316
Report Number: JSC-CN-8316
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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