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Study of selected thrust vector control systems for solid propellant motors final report, 2 Jun. - 2 Aug. 1965Thrust vector control for solid propellant rocket engines - liquid injection system, hot or cold gas systems, and gimballed nozzle systems
Document ID
19660001347
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 2, 2013
Publication Date
August 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
SGC-884-FR-1
NASA-CR-67659
Report Number: SGC-884-FR-1
Report Number: NASA-CR-67659
Accession Number
66N10636
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: JPL-951189
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GIMBALLED CONTROL
THRUST VECTOR CONTROL /TVC/
HOT GAS SYSTEM
SOLID PROPELLANT ROCKET ENGINE
LIQUID INJECTION

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