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A Comparison of Energy Conversion Technologies for Space Nuclear Power SystemsA key element of space nuclear power systems is the energy conversion subsystem that converts the nuclear heat into electrical power. Nuclear systems provide a favorable option for missions that require long-duration power in hostile space environments where sunlight for solar power is absent or limited. There are two primary nuclear power technology options. Radioisotope Power System (RPS) utilize the natural decay heat from Pu238 to generate electric power levels up to about one kilowatt. Fission Power System (FPS) rely on a sustained fission reaction of U235 and offer the potential to supply electric power from kilowatts to megawatts. Example missions for nuclear power include Mars science rovers (e.g. Curiosity, Mars 2020), lunar and Mars surface landers ? including crewed missions, deep space planetary orbiters, Ocean World science landers, and robotic space probes that utilize nuclear electric propulsion. This paper examines the energy conversion technology options that can be used with RPS and FPS, and provides an assessment of their relative performance and technology readiness.
Document ID
20180005431
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
External Source(s)
Authors
Mason, Lee S.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 21, 2018
Publication Date
July 9, 2018
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN57836
AIAA–2018–4977
Meeting Information
Meeting: 2018 AIAA Propulsion and Energy Forum
Location: Cincinnati, OH
Country: United States
Start Date: July 9, 2018
End Date: July 11, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: WBS 600566.01.10.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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