SAE Technical Paper Series 2004
DOI: 10.4271/2004-01-2594
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International Space Station (ISS) Airlock Crewlock Depressurization Methods

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Cited by 4 publications
(9 citation statements)
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“…Crewlock dimensions, operations, and depressurization details are taken from D. E. Williams et al. (2004) while air quality requirements that we use to estimate maximum potential contaminant masses are taken from Table 32 of Wieland (1998). We assume, based upon these references, that the cabin air used in the crewlock during egress will be the sourced from the main cabin air supply, and will thus contain human and mechanical contaminants that are bounded by the prescribed limits.…”
Section: Capturing Key Processes On the Moonmentioning
confidence: 99%
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“…Crewlock dimensions, operations, and depressurization details are taken from D. E. Williams et al. (2004) while air quality requirements that we use to estimate maximum potential contaminant masses are taken from Table 32 of Wieland (1998). We assume, based upon these references, that the cabin air used in the crewlock during egress will be the sourced from the main cabin air supply, and will thus contain human and mechanical contaminants that are bounded by the prescribed limits.…”
Section: Capturing Key Processes On the Moonmentioning
confidence: 99%
“…The PSR source infall and depletion data on which this PSRWT calculations are based is from Farrell et al (2015bFarrell et al ( , 2019, Johnson (1990), andPokorný et al (2019), UV loss rate data from DeSimone and Orlando ( 2015), and thermal desorption data from Andreas (2007) and Pokorný et al (2019). Airlock case study data on depressurization details are taken from D. E. Williams et al (2004) and maximum potential contaminant masses from Wieland (1998). The SDTrimSP code used for the material testing/particle sputtering case study is available at Mutzke et al (2019).…”
Section: Data Availability Statementmentioning
confidence: 99%
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