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Orion Post Landing LiOH and Toxic Sensor DevelopmentThe Orion Crew Exploration Vehicle (CEV) lands in the water with most resources depleted. There is a need to provide CO2 control while the cabin remains sealed for two hours post landing and there is a need to verify the outside air is free of ammonia or propellants, which may be venting from the vehicle, prior to opening the cabin. Development of approaches to perform these tasks while minimizing weight, volume, and cost are being investigated. This paper will document the results of those investigations.
Document ID
20100042582
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
Lewis, John F.
(NASA Johnson Space Center Houston, TX, United States)
Barido, Richard A.
(NASA Johnson Space Center Houston, TX, United States)
Graf, John C.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2010
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-22127
Report Number: JSC-CN-22127
Meeting Information
Meeting: International Conference on Environmental Systems (ICES)
Location: Portland, OR
Country: United States
Start Date: July 17, 2011
End Date: July 21, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 644423.06.31.03.12.10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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