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- W830369549 abstract "This paper describes the thermal design for the propulsion module subsystem (PMS), and presents the results from the radioisotope thermoelectric generator (RTG) waste heat thermal test, and it summarizes the adjustment techniques and their relative effectiveness; it also shows the resulting predicted PMS flight temperatures relative to the requirements." @default.
- W830369549 created "2016-06-24" @default.
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- W830369549 date "1994-06-20" @default.
- W830369549 modified "2023-09-26" @default.
- W830369549 title "RTG Waste Heat System for the Cassini Propulsion Module" @default.
- W830369549 hasPublicationYear "1994" @default.
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