Comfort and Heat Control During Extended Space Flights

961538

07/01/1996

Event
International Conference On Environmental Systems
Authors Abstract
Content
The inability to adequately assess overall temperature in contradictory thermal conditions is problematic for monitoring the safety and comfort of the astronaut during extended EVA. A nonuniform heating/cooling system applied to the surface of the body provides a paradigm for identifying the most sensitive areas for measuring overall heat status. Manipulating warming /cooling tube patterns in the space suit during EVA has potential in providing a normal heat topography. Systematically varying astronaut's heat exchange onboard can enhance comfort and performance and prevent health problems that accompany living in a closely-controlled, constant environmental habitat.
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Details
DOI
https://doi.org/10.4271/961538
Pages
8
Citation
Koscheyev, V., Greaves, I., Leon, G., Hubel, A. et al., "Comfort and Heat Control During Extended Space Flights," SAE Technical Paper 961538, 1996, https://doi.org/10.4271/961538.
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Publisher
Published
Jul 1, 1996
Product Code
961538
Content Type
Technical Paper
Language
English