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Investigation of advanced regenerative thrust chamber designs Final reportFabrication and thermal performance of regeneratively cooled fluorine hydrogen thrust chamber
Document ID
19710004660
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stubbs, V. R. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 2, 2013
Publication Date
November 15, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72742
Report Number: NASA-CR-72742
Accession Number
71N14135
Funding Number(s)
CONTRACT_GRANT: NAS3-7971
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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