航天器
热电发电机
冥王星
航空航天工程
发电机(电路理论)
航空学
天体生物学
伽利略(卫星导航)
环境科学
物理
功率(物理)
热电效应
电气工程
工程类
遥感
地质学
热力学
量子力学
作者
Gary L. Bennett,J.J. Lombardo,Richard J. Hemler,Gil Silverman,C. W. Whitmore,W.R. Amos,Ernest W. Johnson,R.W. Zocher,J. C. Hagan,R.W. Englehart,Mohamed S. El‐Genk
出处
期刊:Nucleation and Atmospheric Aerosols
日期:2008-01-01
被引量:25
摘要
The General‐Purpose Heat Source Radioisotope Thermoelectric Generator (GPHS‐RTG) was developed for the originally planned International Solar Polar Mission (ISPM). [ISPM would later, with the elimination of the NASA spacecraft, become the Ulysses mission.] At 300 We beginning‐of‐life (BOL) power, the GPHS‐RTG was the most powerful RTG with the highest specific power (5.3 We/kg) of any space RTG. These improved performance attributes of the GPHS‐RTG made it attractive for use on the Galileo mission. Subsequently, the GPHS‐RTG was selected to power the Cassini spacecraft, which is currently orbiting Saturn, and the New Horizons spacecraft which is on its way to Pluto. Truly, the GPHS‐RTG is a "general‐purpose" space RTG.
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