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Design and application of self-cooled rocket nozzles Final report, 5 Jan. 1968 - 31 Oct. 1969Design optimum zinc infiltrated self cooled nozzle inserts for hybrid propellant rocket motors
Document ID
19700005828
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schwarzkopf, P. (Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-66861
R-8057
Report Number: NASA-CR-66861
Report Number: R-8057
Accession Number
70N15132
Funding Number(s)
CONTRACT_GRANT: NAS1-7741
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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