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An experimental evaluation of 100-lb-thrust ablatively cooled rocket enginesTest firing of 100-lb thrust ablatively cooled rocket chambers
Document ID
19660028515
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Porter, R. N. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Tyler, W. H. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
October 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
JPL-TR-32-978
NASA-CR-78440
Report Number: JPL-TR-32-978
Report Number: NASA-CR-78440
Accession Number
66N37805
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET CHAMBER
TEST FIRING
ABLATION

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