Shuttle Launch Entry Suit Liquid Cooling System Thermal Performance

Paper #:
  • 951546

Published:
  • 1995-07-01
Citation:
Bue, G., Conger, B., Hooper, P., Chang, C. et al., "Shuttle Launch Entry Suit Liquid Cooling System Thermal Performance," SAE Technical Paper 951546, 1995, https://doi.org/10.4271/951546.
Pages:
13
Abstract:
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.
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