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Integrated Orbiter/International Space Station Air Quality Analysis for Post-Mission 2A.1 Risk MitigationEven under the assumption that all Orbiter and ISS elements would be operating as designed, condensation control and crewmember comfort were paramount issues preceding each of the ISS Missions 2A and 2A.1. However, crewmember discomfort during Mission 2A.1, in addition to evidence provided by flight data and observations, suggested that countermeasures would be necessary for future flights where the Orbiter provides primary control. A review of Space Shuttle Program (SSP) and International Space Station Program (ISSP) assumptions and analytical methods that describe ECLS transport phenomena was accomplished in order to ensure the veracity of future analyses. Subsequently, various analyses and interpretations of Mission 2A.1 flight data provided the necessary information to help understand the probable causes of the flight environment. With cooperation between the SSP and ISSP, countermeasures were devised for Mission 2A.2 that would likely improve the delivery of conditioned air by the Orbiter to the ISS as well as within the ISS elements.
Document ID
20010080071
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Dunaway, Brian
(Boeing Co. Huntsville, AL United States)
Tsai, Ching-Fen
(Boeing Co. Huntsville, AL United States)
Turner, Edward
(Boeing Co. Huntsville, AL United States)
Edeen, Marybeth
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
August 20, 2013
Publication Date
July 1, 2000
Subject Category
Man/System Technology And Life Support
Report/Patent Number
JSC-CN-6194
SAE Paper 2000-01-2250
Distribution Limits
Public
Copyright
Other
Keywords
RISK MANAGEMENT

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