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Design and development of the quad redundant servoactuator for the space shuttle solid rocket booster thrust vector controlThe design and theory of operation of the servoactuator used for thrust vector control of the space shuttle solid rocket booster is described accompanied by highlights from the development and qualification test programs. Specific details are presented concerning major anomalies that occurred during the test programs and the corrective courses of action pursued.
Document ID
19800015016
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lominick, J. M. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 10, 2013
Publication Date
May 1, 1980
Publication Information
Publication: NASA. Langley Res. Center Proc. of the 14th Aerospace Mech. Symp.
Subject Category
Spacecraft Propulsion And Power
Accession Number
80N23507
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19800015004Collected WorksProceedings of the 14th Aerospace Mechanisms Symposium
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