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Thermionic spacecraft design study, 120 kw nuclear electric propulsion system. Volume 1: SummaryElectrically propelled spacecraft designs using thermionic reactors as electrical power source investigated for Halley Comet rendezvous mission
Document ID
19710027901
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 2, 2013
Publication Date
June 30, 1971
Subject Category
Propulsion Systems
Report/Patent Number
GESP-648-VOL-1
NASA-CR-122928
Report Number: GESP-648-VOL-1
Report Number: NASA-CR-122928
Accession Number
71N37377
Funding Number(s)
CONTRACT_GRANT: JPL-952381
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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