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Proportional solid propellant secondary injection thrust vector control studyProportional hot gas secondary injection thrust vector control system for high energy solid propellant rocket motor
Document ID
19670003429
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 3, 2013
Publication Date
November 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-637
Report Number: NASA-CR-637
Accession Number
67N12758
Funding Number(s)
CONTRACT_GRANT: NAS1-2962
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROPORTIONAL CONTROL
GAS INJECTION
HOT GAS SYSTEM
THRUST VECTOR CONTROL /TVC/
SOLID PROPELLANT ROCKET ENGINE

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