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Heat pipe technology for advanced rocket thrust chambersRegenerative cooling system design for rocket engines
Document ID
19710029269
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rousar, D. C. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 15, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-123117
REPT-697-F
Report Number: NASA-CR-123117
Report Number: REPT-697-F
Accession Number
71N38745
Funding Number(s)
CONTRACT_GRANT: NAS7-697
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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