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Title: RTG Waste Heat System for the Cassini Propulsion Module
Authors: Mireles, V.
Stultz, J.
Issue Date: 20-Jun-1994
Citation: Germany
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.
Appears in Collections:JPL TRS 1992+

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