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X-38 Bolt Retractor Subsystem Separation DemonstrationThe Flight Robotics Laboratory FRL successfully demonstrated the X-38 bolt retractor subsystem (BRS). The BRS design was proven safe by testing in the Pyrotechnic Shock Facility (PSI) before being demonstrated in the FRL. This Technical Memorandum describes the BRS, FRL, PSF, and interface hardware. Bolt retraction time, spacecraft simulator acceleration, and a force analysis are also presented. The purpose of the demonstration was to show the FRL capability for spacecraft separation testing using pyrotechnics. Although a formal test was not performed due to schedule and budget constraints, the data will show that the BRS is a successful design concept and the FRL is suitable for future separation tests.
Document ID
20020086933
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Rugless, Fedoria
(NASA Marshall Space Flight Center Huntsville, AL United States)
Johnston, A. S.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Ahmed, R.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Garrison, J. C.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Gaines, J. L.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Waggoner, J. D.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2002
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M-1057
NASA/TM-2002-212047
NAS 1.15:212047
Report Number: M-1057
Report Number: NASA/TM-2002-212047
Report Number: NAS 1.15:212047
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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