1996
DOI: 10.1063/1.50066
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Design of RTPV generators integrated with new millennium spacecraft for outer solar system

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Cited by 6 publications
(9 citation statements)
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“…The RTG uses a thermocouple array to convert this decay heat through the Seebeck effect . The General Purpose Heat Source (GPHS) using Plutonium‐238 ( 238 PuO 2 ) is a modular component of an RTG and was used for NASA spacecraft such as Voyager, New Horizon, and Curiosity Rover. The GPHS‐RTG generates electric power by converting the α decay heat of 238 Pu into electrical energy using a thermoelectric array; however, the system has a low conversion efficiency of 6 to 7% .…”
Section: Introductionmentioning
confidence: 99%
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“…The RTG uses a thermocouple array to convert this decay heat through the Seebeck effect . The General Purpose Heat Source (GPHS) using Plutonium‐238 ( 238 PuO 2 ) is a modular component of an RTG and was used for NASA spacecraft such as Voyager, New Horizon, and Curiosity Rover. The GPHS‐RTG generates electric power by converting the α decay heat of 238 Pu into electrical energy using a thermoelectric array; however, the system has a low conversion efficiency of 6 to 7% .…”
Section: Introductionmentioning
confidence: 99%
“…The General Purpose Heat Source (GPHS) using Plutonium‐238 ( 238 PuO 2 ) is a modular component of an RTG and was used for NASA spacecraft such as Voyager, New Horizon, and Curiosity Rover. The GPHS‐RTG generates electric power by converting the α decay heat of 238 Pu into electrical energy using a thermoelectric array; however, the system has a low conversion efficiency of 6 to 7% . A high fuel inventory with a low conversion efficiency is required to meet a required amount of electricity output, without which there will be inefficiency in spacecraft launch.…”
Section: Introductionmentioning
confidence: 99%
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