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Refractory thrust chambers for spacecraft engines Final reportStructural reliability tests on pyrolytic graphite and pyrolytic graphite alloys for use in liquid propellant rocket engine thrust chambers and nozzles
Document ID
19660003585
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Campbell, J. G. (Marquardt Corp. Van Nuys, CA, United States)
Coulbert, C. D. (Marquardt Corp. Van Nuys, CA, United States)
Date Acquired
August 3, 2013
Publication Date
March 22, 1965
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-68183
Report Number: NASA-CR-68183
Accession Number
66N12874
Funding Number(s)
CONTRACT_GRANT: NAS7-262
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET NOZZLE
STRUCTURAL RELIABILITY
PYROLYTIC GRAPHITE
LIQUID PROPELLANT ROCKET ENGINE

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