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Space Station benefits from ECLS - Propulsion system synergismBenefits of integrating the Space Station Environmental Control and Life Support (ECLS) system with the propulsion system are addressed in this paper for various levels of ECLS closure. Effluents generated by the ECLS system are used to augment or even supplement the propulsion system. Potential benefits include reductions in logistic weights and volumes, fixed weights and volumes, power requirements, and in total station systems cost.
Document ID
19860057881
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brennan, S. M.
(Boeing Aerospace Co. Huntsville, AL, United States)
Donovan, R. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 86-1407
Accession Number
86A42619
Funding Number(s)
CONTRACT_GRANT: NAS3-23353
Distribution Limits
Public
Copyright
Other

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