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Space station propulsion-ECLSS interaction studyThe benefits of the utilization of effluents of the Space Station Environmental Control and Life Support (ECLS) system are examined. Various ECLSS-propulsion system interaction options are evaluated and compared on the basis of weight, volume, and power requirements. Annual propulsive impulse to maintain station altitude during a complete solar cycle of eleven years and the effect on station resupply are considered.
Document ID
19870020161
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brennan, Scott M. (Boeing Aerospace Co. Kent, WA, United States)
Date Acquired
September 5, 2013
Publication Date
February 14, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-175093
NAS 1.26:175093
D483-10060-1
Report Number: NASA-CR-175093
Report Number: NAS 1.26:175093
Report Number: D483-10060-1
Accession Number
87N29594
Funding Number(s)
CONTRACT_GRANT: NAS3-23353
PROJECT: RTOP 506-49-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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