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NASA NTRS1994

RTG Waste Heat System for the Cassini Propulsion Module

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.

Cassini thermal design propulsion module subsystem↗