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Lunar Module Thermal Control and Life Support Systems for Apollo Applications
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English
Abstract
A derivative of the Apollo Lunar Module is being developed to support the operation of a manned, earth orbiting solar observatory. Its thermal control and life support systems demonstrate how previously developed technology and hardware are satisfying mission requirements which differ significantly from those for which the vehicle was originally designed.
Thermal control is accomplished by active and passive means. The active portion of the system employs liquid heat transport and rejection networks. Insulation systems, thermal coatings, and conductive couplings are used as much as is practical to minimize the effects on the vehicle of variations in the external thermal environment. The Apollo Lunar Module life support system has been extensively modified to permit both shirtsleeve and extravehicular crew activities.
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Citation
Renman, R. and Mendelsohn, A., "Lunar Module Thermal Control and Life Support Systems for Apollo Applications," SAE Technical Paper 690625, 1969, https://doi.org/10.4271/690625.Also In
References
- Bartilucci, A. Lee, E. Tawil, M. N. “LM Passive Thermal Design and Test.” AIAA Paper No. 68–748 June 24 1968
- Tawil M. N. Calager, P. “The Use of Multilayer Insulation on the LM Vehicle.” AIAA Paper No. 69–609 June 16 1969
- Leng, J. Oman, R. Hopkins, H. “A Detonation Tube Technique for Simulating Rocket Plumes in a Space Environment.” J. Spacecraft and Rockets 5 10 October 1968
- Royce, L. “AAP/LM-A Radiator Integration Studies.” GAEC Sept. 15 1697