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Challenges in the development of the orbiter atmosphere revitalization subsystemThe space shuttle orbiter atmospheric revitalization subsystem provides thermal and contaminant control as well as total- and oxygen partial-pressure control of the environment within the orbiter crew cabin. Challenges that occurred during the development of this subsystem for the space shuttle orbiter are described. The design of the rotating hardware elements of the system (pumps, fans, etc.) required significant development to meet the requirements of long service life, maintainability, and high cycle-fatigue life. As a result, a stringent development program, particularly in the areas of bearing life and heat dissipation, was required. Another area requiring significant development was cabin humidity control and condensate collection.
Document ID
19850008611
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Prince, R. N.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Swider, J.
(Hamilton Standard Windsor Locks, Conn., United States)
Wojnarowski, J.
(Hamilton Standard Windsor Locks, Conn., United States)
Decrisantis, A.
(Hamilton Standard Windsor Locks, Conn., United States)
Ord, G. R.
(Moog, Inc., East Aurora N.Y., United States)
Walleshauser, J. J.
(Moog, Inc., East Aurora N.Y., United States)
Gibb, J. W.
(Rockwell International Corp. Downey, Calif., United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: Space Shuttle Tech. Conf., Pt. 1
Subject Category
Space Transportation
Accession Number
85N16920
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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