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Nuclear electric power for multimegawatt orbit transfer vehiclesMultimegawatt nuclear propulsion is an attractive option for orbit transfer vehicles. The masses of these platforms are expected to exceed the capability of a single launch from Earth necessitating assembly in space in a parking orbit. The OTV would transfer the platform from the parking orbit to the operational orbit and then return for the next mission. Electric propulsion is advantageous because of the high specific impulse achieved by the technology, 1000 to 5000 s and beyond, to reduce the propellant required. Nuclear power is attractive as the power system because of the weight savings over solar systems in the multimegawatt regime, and multimegawatts of power are required. A conceptual diagram is shown of an OTV with a command control module using electric thrusters powered from an SP-100 class nuclear reactor power system.
Document ID
19880014877
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Casagrande, R. D.
(General Electric Co. Philadelphia, PA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Publication Information
Publication: New Mexico Univ., Transactions of the Fourth Symposium on Space Nuclear Power Systems
Subject Category
Electronics And Electrical Engineering
Accession Number
88N24261
Funding Number(s)
CONTRACT_GRANT: F29601-86-C-0238
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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