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Shuttle Orbiter Environmental Control and Life Support System - Flight experienceThis paper describes the overall design of the Shuttle Orbiter Environmental Control and Life Support System (ECLSS). The Orbiter ECLSS consists of six major subsystems which accomplish the functions of providing a habitable pressurized cabin atmosphere and removing gaseous contaminants, controlling the temperature of the cabin and vehicle components within acceptable ranges, providing fire detection and suppression capability, maintaining a supply of potable water, collecting and removing metabolic waste materials, and providing utilities and access for extravehicular activity. The operational experience is summarized for the 45 space flights accomplished to date during which the Orbiter ECLSS has been demonstrated to perform reliably, and has proved to have the flexibility to meet a variety of mission needs. Significant flight problems are described, along with the design or procedure changes which were implemented to resolve the problems.
Document ID
19930057510
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Winkler, H. E.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 16, 2013
Publication Date
July 1, 1992
Subject Category
Man/System Technology And Life Support
Report/Patent Number
SAE PAPER 921348
Meeting Information
Meeting: SAE, International Conference on Environmental Systems
Location: Seattle, WA
Country: United States
Start Date: July 13, 1992
End Date: July 16, 1992
Sponsors: SAE
Accession Number
93A41507
Distribution Limits
Public
Copyright
Other

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