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Investigation into Venting and Non-venting Technologies for the Space Station Freedom Extravehicular Activity Life Support System

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Wilson, John L., author.
Conference Name:
International Conference On Environmental Systems (1990-07-09 : Williamsburg, Virginia, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1990
Summary:
During the continuing effort to design the Space Station Freedom extravehicular activity (EVA) life support system, NASA has extensively researched and evaluated venting and non-venting technologies. In conducting this study, NASA has concentrated on a system-level approach that emphasizes on-orbit regeneration capabilities, minimization of expendables, minimal on-orbit maintenance requirements, a four to eight hour EVA capacity, and a system weight and volume close to the Space Shuttle unit. This paper will describe various venting and non-venting technologies and review the estimated weights and volumes for the options on a component and system level. At this time, a final design concept for the Space Station extravehicular mobility unit has not been chosen
Notes:
Vendor supplied data
Publisher Number:
901319
Access Restriction:
Restricted for use by site license

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