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Shuttle Launch Entry Suit Liquid Cooling System Thermal Performance Lockheed Engrg. and Sciences Company

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Bue, Grant C., author.
Conference Name:
International Conference on Environmental Systems (1995-07-10 : San Diego, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1995
Summary:
A thermoelectric liquid cooling system recently developed at the Johnson Space Center was evaluated in manned and unmanned ground tests as an alternative to the Space Shuttle launch and entry suit personal fan. The liquid cooling system provided superior cooling in environments simulating flight deck conditions during launch and postlanding
Notes:
Vendor supplied data
Publisher Number:
951546
Access Restriction:
Restricted for use by site license

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