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Research and development of a vortex valve controlled hot gas /5500 deg F/ secondary injection thrust vector control systemPerformance of vortex valve controlled secondary injection thrust vector system for solid propellant rocket motor control
Document ID
19680027152
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Blatter, A. (Bendix Corp. Southfield, MI, United States)
Keranen, T. W. (Bendix Corp. Southfield, MI, United States)
Date Acquired
August 4, 2013
Publication Date
September 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
BRL-4455
NASA-CR-66692
Report Number: BRL-4455
Report Number: NASA-CR-66692
Accession Number
68N36624
Funding Number(s)
CONTRACT_GRANT: NAS1-5199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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