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Stability characterization of advanced injectors, design guide. Volume 2 - Operation of the computer program, Phase 3 Final reportComputerized stability design of time lag combustion system for liquid propellant rocket engine
Document ID
19710010940
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Waugh, R. C. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
August 6, 2013
Publication Date
February 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-120096
REPT-20672-P3D-REV-A
Report Number: NASA-CR-120096
Report Number: REPT-20672-P3D-REV-A
Accession Number
71N20415
Funding Number(s)
CONTRACT_GRANT: NAS8-20672
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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