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A Deep Space Power System Option Based on Synergistic Power Conversion TechnologiesDeep space science missions have typically used radioisotope thermoelectric generator (RTG) power systems. The RTG power system has proven itself to be a rugged and highly reliable power system over many missions, however the thermal-to-electric conversion technology used was approximately 5% efficient. While the relatively low efficiency has some benefits in terms of system integration, there are compelling reasons why a more efficient conversion system should be pursued. The cost savings alone that are available as a result of the reduced isotope inventory are significant. The Advanced Radioisotope Power System (ARPS) project was established to fulfill this goal. Although it was not part of the ARPS project, Stirling conversion technology is being demonstrated with a low level of funding by both NASA and DOE. A power system with Stirling convertors. although intended for use with an isotope heat source. can be combined with other advanced technologies to provide a novel power system for deep space missions. An inflatable primary concentrator would be used in combination with a refractive secondary concentrator (RSC) as the heat source to power the system. The inflatable technology as a structure has made great progress for a variety of potential applications such as communications reflectors, radiators and solar arrays. The RSC has been pursued for use in solar thermal propulsion applications, and it's unique properties allow some advantageous system trades to be made. The power system proposed would completely eliminate the isotope heat source and could potentially provide power for science missions to planets as distant as Uranus. This paper will present the background and developmental status of the technologies and will then describe the power system being proposed.
Document ID
20000085858
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Schreiber, Jeffrey G.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2000
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TM-2000-210232
NAS 1.15:210232
E-12352
Meeting Information
Meeting: 2000 Space Technoogy and Applicatins International Forum
Location: Albuquerque, NM
Country: United States
Start Date: January 30, 2000
End Date: February 3, 2000
Sponsors: American Inst. of Physics
Funding Number(s)
PROJECT: RTOP 839-20-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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