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    The X-38 V-201 Flap Actuator Mechanism (2004)
    In:  CASI
    Details
    Publication Date: 2018-06-11
    Description: The X-38 Crew Rescue Vehicle V-201 space flight test article was designed to achieve an aerodynamically controlled re-entry from orbit in part through the use of two body mounted flaps on the lower rear side. These flaps are actuated by an electromechanical system that is partially exposed to the re-entry environment. These actuators are of a novel configuration and are unique in their requirement to function while exposed to re-entry conditions. The authors are not aware of any other vehicle in which a major actuator system was required to function throughout the complete re-entry profile while parts of the actuator were directly exposed to the ambient environment.
    Keywords: Spacecraft Design, Testing and Performance
    Type: 37th Aerospace Mechanisms Symposium; 377-390; NASA/CP-2004-212073
    Format: application/pdf
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