Thermal Technologies for Space Suits

ASHRAE Journal

Volumn 43, Issue 1, 2001, Pages 25-36

  Mays, Darrell Craig ^a   Campbell, Anthony B ^a   Nair, Satish S ^b   Miles, John B ^c   Thomas, Gretchen A ^d  

^a HONEYWELL   (United States)

^b University of Missouri   (United States)

^c UNIVERSITY OF MISSOURI   (United States)

^d NASA JOHNSON SPACE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC PRESSURE; CARBON DIOXIDE; EARTH ATMOSPHERE; MANNED SPACE FLIGHT;

DEBRIS IMPACTS; EFFECTIVE TEMPERATURE; EXTRA VEHICULAR ACTIVITIES; LOW PRESSURES; MARTIAN ATMOSPHERES; PRIMARY FACTORS; SPACE SUIT; THERMAL TECHNOLOGIES;

SPACE DEBRIS;

EID: 0002133781     PISSN: 00012491     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (9)

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2. McBarron II, J.W., et al. 1991. "Individual systems for crewmember life support and extravehicular activity." Space Biology and Medicine. American Institute of Aeronautics and Astronautics.
3. Balinskas, R., Tepper, E. 1992. Extravehicular Mobility Unit Requirements and Evolution, United Technologies, Hamilton Standard, NAS 9-17873.
4. Lawson, M., C. Cross. 1998. "The advanced spacesuit project -97 update." 28'h International Conference on Environmental Systems, SAE 981629.
5. Cross, C. 1998. RAD Development Test Results, Houston: National Aeronautics and Space Administration, Johnson Space Center.
6. Mays, D.C., et al. 1999. "Design of a transient thermal model of the cryogenic PLSS." 29th International Conference on Environmental Systems. SAE 1999-01-2000.
7. Campbell, A.B. et al. 1999. "Dynamic modeling of the minimum consumables PLSS." 29"" International Conference on Environmental Systems. SAE 1999-02-2000.
8. Jones, E.M. 1995.Apollo 17 Lunar Surface Journal PLSS Technical Information, www.nasa.gov.
9. rd International Conference on Environmental Systems. SAE 93223.