Thermal Control System for Space Station Freedom Photovoltaic Power Module

921110

07/01/1992

Event
International Conference On Environmental Systems
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/921110
Pages
13
Citation
Hacha, T., and Howard, L., "Thermal Control System for Space Station Freedom Photovoltaic Power Module," SAE Technical Paper 921110, 1992, https://doi.org/10.4271/921110.
Additional Details
Publisher
Published
Jul 1, 1992
Product Code
921110
Content Type
Technical Paper
Language
English