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Optimization of System Operating Parameters for Heat Sterilizable Liquid Propulsion SystemsOperating parameters of liquid propulsion systems capable of being heat sterilized in loaded condition without venting
Document ID
19660021468
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Curtis, H. D. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Harper, A. D. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
June 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-76318
JPL-TM-33-211
Report Number: NASA-CR-76318
Report Number: JPL-TM-33-211
Accession Number
66N30758
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID PROPELLANT
PROPULSION SYSTEM
SPACECRAFT STERILIZATION
HEAT TREATMENT

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