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Feasibility study of LITVC for shuttle SRBA liquid injection thrust vector control (LITVC) system for the shuttle solid rocket booster (SRB) was analyzed. The LITVC was compared with the SRB baseline flexible seal. A table of LITVC advantages and disadvantages is presented. It is concluded that the LITVC performs well at low to moderate duty cycles, but not for high duty cycle requirements.
Document ID
19810024688
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Martin, C. L. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Powers, L. B. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TP-1912
M-354
Accession Number
81N33231
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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