The electric power for Space Station Freedom (SSF) is generated by the solar arrays of the photo-voltaic power modules (PVM's) and conditioned, controlled, and distributed by a power management and distribution system. The PVM's are located outboard of the alpha gimbals of SSF. A single-phase thermal control system is being developed to provide thermal control of PVM electrical equipment and energy storage batteries. This system uses ammonia as the coolant and a direct-flow deployable radiator. This paper presents the description and development status of the PVM thermal control system.
Thermal Control System for Space Station Freedom Photovoltaic Power Module
Sae Technical Papers
International Conference On Environmental Systems ; 1992
01.07.1992
Aufsatz (Konferenz)
Englisch
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