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The development of a non-cryogenic nitrogen/oxygen supply systemA hydrazine/water electrolysis process system module design was fabricated and tested to demonstrate component and module performance. This module is capable of providing both the metabolic oxygen for crew needs and the oxygen and nitrogen for spacecraft leak makeup. The component designs evolved through previous R and D efforts, and were fabricated and tested individually and then were assembled into a complete module which was successfully tested for 1000 hours to demonstrate integration of the individual components. A survey was made of hydrazine sensor technology and a cell math model was derived.
Document ID
19740023468
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Greenough, B. M.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Mahan, R. E.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1974
Subject Category
Biotechnology
Report/Patent Number
NASA-CR-134390
LMSC-D401948
Accession Number
74N31581
Funding Number(s)
CONTRACT_GRANT: NAS9-13051
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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