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Boeing Crew Exploration Vehicle Environmental Control & Life Support System Architecture Overview
Technical Paper
2007-01-3043
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
The Boeing Company under the teaming agreement with the Northrop Grumman Systems Corporation and in compliance with the NASA Phase 1 contract had the responsibilities for the CEV architecture development of the Environmental Control and Life Support (ECLS) system under the NASA Phase 1 contract. The ECLS system was comprised of the various subsystems which provided for a shirt-sleeve habitable environment for crew to live and work in the crew module of the CEV. This architecture met the NASA requirements to ferry cargo and crew to ISS, and Lunar sortie missions, with extensibility to long duration missions to Moon and Mars. This paper provides a summary overview of the CEV ECLS subsystems which was proposed in compliance with the contract activities.
Authors
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Citation
Saiidi, M. and Lewis, J., "Boeing Crew Exploration Vehicle Environmental Control & Life Support System Architecture Overview," SAE Technical Paper 2007-01-3043, 2007, https://doi.org/10.4271/2007-01-3043.Also In
References
- System Requirements For The Crew Exploration Vehicle Element February 03 2006
- Lewis John F. Crew Exploration Vehicle Environmental Control and Life Support Development Status