NASA NTRS · 19800015016
Design and development of the quad redundant servoactuator for the space shuttle solid rocket booster thrust vector control
Abstract
The 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.
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Lominick, J. M.. 1980-05-01. Design and development of the quad redundant servoactuator for the space shuttle solid rocket booster thrust vector control. https://ntrs.nasa.gov/citations/19800015016
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