NASA NTRS · 19930007530
Reusable Reentry Satellite (RRS): Thermal control trade study
Abstract
The design and assessment work performed in defining the on-orbit Thermal Control Subsystem (TCS) requirements for the Reusable Reentry Satellite (RRS) is discussed. Specifically, it describes the hardware and design measures necessary for maintaining the Payload Module (PM) Environmental Control Life Support System (ECLSS) heat exchanger, the hydrazine propellant, and PM water supply within their required temperature limits.
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Wallace, Clark. 1990-04-01. Reusable Reentry Satellite (RRS): Thermal control trade study. https://ntrs.nasa.gov/citations/19930007530
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