2018-07-082018-07-082018-07-08ICES_2018_325http://hdl.handle.net/2346/74259Stojan Madzunkov, Jet Propulsion LaboratorySteven Schowalter, Jet Propulsion LaboratoryDragan Nikolic, Jet Propulsion LaboratoryJurij Simcic, Jet Propulsion LaboratoryByunghoon Bae, Jet Propulsion LaboratoryIvan Cisneros, Jet Propulsion LaboratoryRembrandt Schaefer, Jet Propulsion LaboratoryMurray Darrach, Jet Propulsion LaboratoryICES205: Advanced Life Support Sensor and Control TechnologyThe 48th International Conference on Environmental Systems was held in Albuquerque, New Mexico, USA on 08 July 2018 through 12 July 2018.The 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.engMass SpectrometryGas ChromatographyMicro-Electro-Mechanical SystemProgress Report on the Spacecraft Atmosphere Monitor’s Development ModelPresentation