Progress Report on the Spacecraft Atmosphere Monitor’s Development Model

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dc.creatorMadzunkov, Stojan
dc.creatorSchowalter, Steven
dc.creatorNikolic, Dragan
dc.creatorSimcic, Jurij
dc.creatorBae, Byunghoon
dc.creatorCisneros, Ivan
dc.creatorSchaefer, Rembrandt
dc.creatorDarrach, Murray
dc.date.accessioned2018-07-08T03:19:25Z
dc.date.available2018-07-08T03:19:25Z
dc.date.issued2018-07-08
dc.descriptionStojan Madzunkov, Jet Propulsion Laboratory
dc.descriptionSteven Schowalter, Jet Propulsion Laboratory
dc.descriptionDragan Nikolic, Jet Propulsion Laboratory
dc.descriptionJurij Simcic, Jet Propulsion Laboratory
dc.descriptionByunghoon Bae, Jet Propulsion Laboratory
dc.descriptionIvan Cisneros, Jet Propulsion Laboratory
dc.descriptionRembrandt Schaefer, Jet Propulsion Laboratory
dc.descriptionMurray Darrach, Jet Propulsion Laboratory
dc.descriptionICES205: Advanced Life Support Sensor and Control Technology
dc.descriptionThe 48th International Conference on Environmental Systems was held in Albuquerque, New Mexico, USA on 08 July 2018 through 12 July 2018.
dc.description.abstractThe Spacecraft Atmosphere Monitor (S.A.M.) is a miniature gas chromatograph (GC) mass spectrometer (MS) intended for assessing trace volatile organic compounds and the major constituents in the atmosphere of present (the International Space Station) and future crewed spacecraft. As such, S.A.M. will continuously sample concentrations of major air constituents (CH4, H2O, N2, O2, and CO2) and report results in two-second intervals. The S.A.M. is a technology demonstration planned to be delivered in February 2019 and consequently launched in May 2019. The S.A.M. is mechanically designed to operate under hi-G loads present during launch events and can operate at sub-atmospheric pressures relevant to extra-vehicular activities. Total instrument mass is projected at 9.5 kg with power consumption estimated at 35 W. The S.A.M. instrument will provide on-demand reporting on trace volatile organic compounds (VOC) at ppm to ppb levels of 21+ species relevant for astronaut health. Here we are reporting on the results from the Development Model (DM) as its being prepared to be deliver to Marshal Space Center for testing and validation.en_US
dc.identifier.otherICES_2018_325
dc.identifier.urihttp://hdl.handle.net/2346/74259
dc.language.isoengen_US
dc.publisher48th International Conference on Environmental Systemsen_US
dc.subjectMass Spectrometry
dc.subjectGas Chromatography
dc.subjectMicro-Electro-Mechanical System
dc.titleProgress Report on the Spacecraft Atmosphere Monitor’s Development Modelen_US
dc.typePresentationen_US

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