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Space Shuttle life support systems - A status reportThe Space Shuttle Program has two independent life support systems. One provides the basic environmental control for the Orbiter cabin while the second enables the crewmen to function outside the spacecraft for extravehicular operation. Although both of these systems were developed and fabricated under contract to NASA, all system-level testing was conducted at the Johnson Space Center. The paper will discuss the results of this testing which, in part, includes: (1) certification of the Orbiter cabin atmospheric pressure and composition control system at three operational pressures (8 psia, 9 psia and 14.7 psia); (2) certification of the Orbiter atmospheric revitalization system at 9 psia and 14.7 psia; (3) manrating of the Orbiter airlock at 14.7 psia, 9 psia and vacuum; and (4) certification of the space suit/life support system in the airlock and at deep space thermal/vacuum conditions. In addition, pertinent flight information from the on-orbit performance of the Shuttle life support systems will be presented.
Document ID
19810062990
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Faget, M. A.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Guy, W. W.
(NASA Johnson Space Center Engineering and Development Directorate Houston, TX, United States)
Date Acquired
August 11, 2013
Publication Date
September 1, 1981
Subject Category
Man/System Technology And Life Support
Report/Patent Number
IAF PAPER 81-181
Accession Number
81A47394
Distribution Limits
Public
Copyright
Other

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