The NASA JSC Shuttle EMU computer model (SINDA EMU) is presently used to analyze the thermal behavior of the Space Shuttle EMU. This paper uses the SINDA EMU model along with EMU experimental and flight data to investigate and define several performance characteristics of the Space Shuttle EMU related to thermal comfort control.
EMU Thermal Performance Characteristics
Sae Technical Papers
International Conference On Environmental Systems ; 1998
1998-07-13
Aufsatz (Konferenz)
Englisch
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