The Technology Demonstration of the Spacecraft Atmosphere Monitor
dc.creator | Schowalter, Steven | |
dc.creator | Madzunkov, Stojan | |
dc.creator | Darrach, Murray | |
dc.creator | Diaz, Ernesto | |
dc.creator | Moore, Brad | |
dc.creator | Simcic, Jurij | |
dc.creator | Nikolic, Dragan | |
dc.creator | Bae, Byunghoon | |
dc.date.accessioned | 2019-06-21T14:24:20Z | |
dc.date.available | 2019-06-21T14:24:20Z | |
dc.date.issued | 2019-07-07 | |
dc.description | Steven Schowalter, Jet Propulsion Laboratory (JPL), USA | |
dc.description | Stojan Madzunkov, Jet Propulsion Laboratory (JPL), USA | |
dc.description | Murray Darrach, Jet Propulsion Laboratory (JPL), USA | |
dc.description | Ernesto Diaz, Jet Propulsion Laboratory (JPL), USA | |
dc.description | Brad Moore, Jet Propulsion Laboratory (JPL), USA | |
dc.description | Jurij Simcic, Jet Propulsion Laboratory (JPL), USA | |
dc.description | Dragan Nikolic, Jet Propulsion Laboratory (JPL), USA | |
dc.description | Byunghoon Bae, Jet Propulsion Laboratory (JPL), USA | |
dc.description | ICES205: Advanced Life Support Sensor and Control Technology | |
dc.description | The 49th International Conference on Environmental Systems as held in Boston, Massachusetts, USA on 07 July 2019 through 11 July 2019. | |
dc.description.abstract | The Spacecraft Atmosphere Monitor (S.A.M.) is a miniaturized Gas Chromatograph Mass Spectrometer (GC/MS) instrument being sent to the International Space Station (ISS) in 2019. While on-station, the S.A.M. instrument will continuously monitor the major atmospheric constituents as well as trace organic volatiles in the cabin air daily. At its core, the S.A.M. sensor consists of a quadrupole ion trap mass spectrometer (QITMS) coupled to a MEMS preconcentrator, gas chromatograph, and microvalve system. Its miniature, ruggedized form factor allows the S.A.M. to be aisle-deployed throughout different nodes of the ISS to monitor different astronaut environments and activities such as exercise and sleep. The final system design of the S.A.M. flight unit, regarding the GC/MS architecture, the mechanical and electrical assembly, and the software implementation, will be discussed in detail and the S.A.M. flight unit performance will be presented. | |
dc.format.mimetype | application/pdf | |
dc.identifier.other | ICES_2019_321 | |
dc.identifier.uri | https://hdl.handle.net/2346/84516 | |
dc.language.iso | eng | |
dc.publisher | 49th International Conference on Environmental Systems | |
dc.subject | Air Monitor | |
dc.subject | International Space Station | |
dc.subject | Quadrupole Ion Trap Mass Spectrometry | |
dc.subject | MEMS Gas Chromatography | |
dc.title | The Technology Demonstration of the Spacecraft Atmosphere Monitor | en_US |
dc.type | Presentations |