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Integrated Air/Water Cooling Concepts for Space Laboratory Modules
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English
Abstract
The advent of permanently operating space laboratories as part of the International Space Station Freedom raises challenging requirements also for the thermal and environmental control of those laboratories.
Enhanced crew size, power dissipation due to a broad range of experiments, flexibility with respect to payload reconfiguration and rack interchangeability, to name only a few, typically are such requirements.
The paper is devoted to the analysis of these requirements and related conceptual design solutions in the light of overall system aspects with special emphasis on the permanently Attached Laboratory of the European Columbus Programme.
In particular the following subjects will be addressed: loops concept factors like parallel /serial /multi loop/single loop and reconfiguration of water cooling and air cooling loops.
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Citation
Sarri, G., Leiseifer, H., and Patti, B., "Integrated Air/Water Cooling Concepts for Space Laboratory Modules," SAE Technical Paper 901370, 1990, https://doi.org/10.4271/901370.Also In
References
- Hienerwadel K.-O. Kring G. “Design of the Environmental Control & Life Support System for the Columbus Pressurized Modules” Paper No. 891531 Intersociety Conference on Environmental Systems San Diego, California July 24-26 1989
- Leiseifer H.P. Hienerwadel K.-O. Patti B. “Air Loop Concepts for Environmental Control and Life Support” Paper No. 891537 Intersociety Conference on Environmental Systems San Diego, California July 24-26 1989
- Aeronautical Radio Inc. 2551 Riva Road, Annapolis, Maryland 21401 “Air Transport Equipment Cases and Racking Arinc Specification 404A” March 15 1974
- “Comparison of Thermal Portions of Arinc Specifications 404A and 600-7 Relative to Space Station Avionics Air Cooling” Marshall George C. Space Flight Center, NASA January 10 1990
- Cushman R. Burke H. “Avionics Air Cooling for Space Station Freedom” Paper No. 891459 Intersociety Conference on Environmental Systems San Diego, California July 24-26 1989
- Sosnay R. “The Spacelab Avionics Loop” Proceedings of Spacecraft Thermal & Environmental Control System Symposium Munich 10-12 October 1978
- Preiss H. Padwater A.D. “The Spacelab Cabin Loop” Proceedings of Spacecraft Thermal & Environmental Control System Symposium Munich 10-12 October 1978