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.
Citation: Campbell, A., Mays, D., Nair, S., Miles, J. et al., "EMU Thermal Performance Characteristics," SAE Technical Paper 981720, 1998, https://doi.org/10.4271/981720. Download Citation
Author(s):
Anthony B. Campbell, D. Craig Mays, Satish S. Nair, John B. Miles, John V. Iovine, Chin H. Lin
Affiliated:
University of Missouri - Columbia
Pages: 15
Event:
International Conference On Environmental Systems
Also in:
SAE 1998 Transactions - Journal of Aerospace-V107-1
