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Space station integrated propulsion and fluid systems studyThe program study was performed in two tasks: Task 1 addressed propulsion systems and Task 2 addressed all fluid systems associated with the Space Station elements, which also included propulsion and pressurant systems. Program results indicated a substantial reduction in life cycle costs through integrating the oxygen/hydrogen propulsion system with the environmental control and life support system, and through supplying nitrogen in a cryogenic gaseous supercritical or subcritical liquid state. A water sensitivity analysis showed that increasing the food water content would substantially increase the amount of water available for propulsion use and in all cases, the implementation of the BOSCH CO2 reduction process would reduce overall life cycle costs to the station and minimize risk. An investigation of fluid systems and associated requirements revealed a delicate balance between the individual propulsion and fluid systems across work packages and a strong interdependence between all other fluid systems.
Document ID
19890005783
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bicknell, B.
(Martin Marietta Aerospace Denver, CO, United States)
Wilson, S.
(Martin Marietta Aerospace Denver, CO, United States)
Dennis, M.
(Martin Marietta Aerospace Denver, CO, United States)
Shepard, D.
(Martin Marietta Aerospace Denver, CO, United States)
Rossier, R.
(Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
MCR-88-539
NASA-CR-183509
NAS 1.26:183509
Report Number: MCR-88-539
Report Number: NASA-CR-183509
Report Number: NAS 1.26:183509
Accession Number
89N15154
Funding Number(s)
CONTRACT_GRANT: NAS8-36438
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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