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Lunar Module Environmental Control Subsystem
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English
Abstract
The lunar module environmental control subsystem provides life support functions, active cooling for the heat loads, and water and oxygen. Featured designs include brushless d-c motors, water sublimators, water-gas centrifugal separators, and cold rail electronics cooling. Testing proceeded incrementally from component development through flight vehicle vacuum chamber demonstrations. Major developments required were the water sublimators, water-gas centrifugal separators, oxygen pressure regulators, and iodine-water compatibility with the system. The flight records of the lunar module environmental control subsystem have been satisfactory.
Authors
Citation
Gillen, R., Elliot, F., and Wilde, R., "Lunar Module Environmental Control Subsystem," SAE Technical Paper 690619, 1969, https://doi.org/10.4271/690619.Also In
References
- Craig Jerry W. “Apollo Spacecraft Nonmetallic Materials Requirements.” Feb. 9 1968