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Space Station propulsion system test bed and control system testing resultsThe test bed fabricated to demonstrate hydrogen/oxygen propulsion technology readiness for the IOC Space Station application is described and test results are presented. The reliability and safety of the O2/H2 system was demonstrated with blowdowns and thruster firings. The flexibility of the system was demonstrated through the addition of an electrolysis supply module.
Document ID
19870057981
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Norman, A. M.
(Rockwell International Corp. Canoga Park, CA, United States)
Briley, G. L.
(Rockwell International Corp. Canoga Park, CA, United States)
Nave, L. H.
(Rockwell International Corp. Canoga Park, CA, United States)
Pavlinsky, J. F.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Allums, S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1987
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
AIAA PAPER 87-1858
Accession Number
87A45255
Funding Number(s)
CONTRACT_GRANT: NAS8-36418
Distribution Limits
Public
Copyright
Other

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