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The X-37 Hot Structure Control Surface TestingThermal-structural testing of three hot structure control surface subcomponent test articles (STA) designed for the X-37 (Boeing Phantom Works, Huntington Beach, California) Orbital Vehicle (OV) has been completed. The test articles were subcomponents of the X-37 OV bodyflap and flaperon control surfaces.
Document ID
20060056099
Acquisition Source
Armstrong Flight Research Center
Document Type
Other
Authors
Hudson, Larry D. (NASA Dryden Flight Research Center Edwards, CA, United States)
Stephens, Craig A. (NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2006
Publication Information
Publication: 2004 Research Engineering Annual Report
Subject Category
General
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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