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Ascent control studies of the 049 and ATP parallel burn solid rocket motor shuttle configurationsThe control authority approach is discussed as a major problem of the parallel burn soil shuttle configuration due to the many resulting system impacts regardless of the approach. The major trade studies and their results, which led to the recommendation of an SRB TVC control authority approach are presented.
Document ID
19730009127
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ryan, R. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Mowery, D. K.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hammer, M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Weisler, A. C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
Space Sciences
Report/Patent Number
NASA-TM-X-64720
Accession Number
73N17854
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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