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Preliminary investigations to determine nuclear-electric spacecraft configurations for high-energy missionsNuclear electric spacecraft configurations effects on mass of spacecraft radiation shield, heat rejection radiators, booster adapter, and aerodynamic shroud subsystems
Document ID
19670020102
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Volkoff, J. J. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Womack, J. R. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
June 15, 1967
Subject Category
Space Vehicles
Report/Patent Number
JPL-TR-32-1085
NASA-CR-84998
Report Number: JPL-TR-32-1085
Report Number: NASA-CR-84998
Accession Number
67N29431
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
WEIGHT FACTOR
RADIATION SHIELDING
SPACECRAFT CONFIGURATION
HEAT REJECTION DEVICE
ELECTRIC PROPULSION

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