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Integration of Thermal and Environmental Control Systems During Space Station Freedom Early Assembly Phase

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Di Pietro, David A., author.
Conference Name:
International Conference On Environmental Systems (1992-07-12 : Seattle, Washington, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1992
Summary:
An overview of Space Station Freedom Thermal Control System (TCS) and Environmental Control and Life Support System (ECLSS) integration is presented for Stages 2-6. Particular attention is given to issues associated with integrating five distinct, functioning spacecraft with hardware not specifically designed for intermediate stages. Areas specifically addressed include integrated ECLSS temperature and humidity control performance, thermal load balancing, performance and verification requirements, interface verification procedures, TCS activation sequence, resource allocation and Space Shuttle integration
Notes:
Vendor supplied data
Publisher Number:
921259
Access Restriction:
Restricted for use by site license

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