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EDC development and testing for the Space Station programNASA's development of electrochemical CO2 concentration technology has led to the creation of subsystem hardware and control and monitoring instrumentation that are ideally suited to Space Station program applications; only seven orbital replacement units, for instance, are required for the performance of process functions. This process simplification leads to superior reliability and enhanced maintainability. Hardware and software features that enhance subsystem reliability through fault detection and isolation have been emphasized in the course of development. Further power, weight, and volume savings, together with enhanced maintainability, are also foreseen in prospective developments of these subsystems.
Document ID
19870051436
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Boyda, R. B.
(Life Systems, Inc. Cleveland, OH, United States)
Hendrix, S. P.
(Life Systems, Inc. Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Man/System Technology And Life Support
Report/Patent Number
SAE PAPER 860918
Accession Number
87A38710
Distribution Limits
Public
Copyright
Other

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