Comfort and Heat Control During Extended Space Flights
961538
07/01/1996
- Event
- 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.
- 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.