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Advanced injector concepts investigation Final reportLiquid propellant rocket engine throttling injector design based on exhaust gas counter flow and heat transfer for inflowing propellant vaporization and combustion stability tests
Document ID
19710018682
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 6, 2013
Publication Date
April 30, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-119796
FR-21052-3F
Report Number: NASA-CR-119796
Report Number: FR-21052-3F
Accession Number
71N28158
Funding Number(s)
CONTRACT_GRANT: NAS8-21052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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