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Stirling radioisotope generator
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Stirling radioisotope generator : ウィキペディア英語版
Stirling radioisotope generator

The Stirling radioisotope generator (SRG) is a generator based on a Stirling engine powered by a large radioisotope heater unit. The hot end of the Stirling converter reaches high temperature and heated helium drives the piston, heat being rejected at the cold end of the engine. A generator or alternator converts the motion into electricity. This Stirling converter produces about four times as much electric power from the plutonium fuel as a radioisotope thermoelectric generator (RTG). The Stirling generators have been extensively tested but have not yet been deployed on actual spacecraft missions.
Stirling engine development began at NASA Glenn Research Center (then NASA Lewis) in the early 1970s. The Space Demonstrator Engine (or SPDE) was the earliest 12.5 kWe per cylinder engine that was designed, built and tested. A later engine of this size, the Component Test Power Converter (or CTPC), used a "Starfish" heat-pipe heater head, instead of the pumped-loop used by the SPDE. In the 1992-93 time period, this work was stopped due to the termination of the related SP-100 nuclear power system work and NASA's new emphasis on "better, faster, cheaper" systems and missions.
==ASRG==
(詳細はAdvanced Stirling Radioisotope Generator (ASRG), a power source based on a 55-watt electric converter.〔(ASRG data sheet ) (NASA Glenn) and (DOE info ). (accessed May 3, 2011)〕〔(NASA Technical Memorandum TM-2007-214806 ) (2007), (accessed May 3, 2011)〕 The thermal power source for this system was the General Purpose Heat Source (GPHS). Each GPHS contained four iridium-clad Pu-238 fuel pellets, stood 5 cm tall, 10 cm square and weighed 1.44 kg. The hot end of the Stirling converter reached 650 °C and heated helium drove a free piston reciprocating in a linear alternator, heat being rejected at the cold end of the engine. The alternating current (AC) generated by the alternator was then converted to 55 watts direct current (DC). Thus each ASRG unit would use two Stirling converter units with about 500 watts of thermal power supplied by two GPHS units and would deliver 100-120 watts of electric power. The ASRG underwent qualification testing at NASA Glenn, as a power supply for a future NASA mission. The ASRG was designed into many mission proposals in this era,〔(B. Berger - Discovery Mission Finalists Could Be Given Second Shot (2014) )〕 but was cancelled in 2013.〔(The ASRG Cancellation in Context ) Future Planetary Exploration〕

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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