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NASA NTRS · 20060056099

The X-37 Hot Structure Control Surface Testing

Abstract

Thermal-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.

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BibTeXRIS

Hudson, Larry D., Stephens, Craig A.. 2006-06-01. The X-37 Hot Structure Control Surface Testing. https://ntrs.nasa.gov/citations/20060056099

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