Optical Multi-Gas Monitor Technology Demonstration on the International Space Station
| dc.creator | Pilgrim, Jeffrey S. | |
| dc.creator | Wood, William R. | |
| dc.creator | Casias, Miguel E. | |
| dc.creator | Vakhtin, Andrei B. | |
| dc.creator | Johnson, Michael D. | |
| dc.creator | Mudgett, Paul D. | |
| dc.date.accessioned | 2014-10-20T18:30:16Z | |
| dc.date.available | 2014-10-20T18:30:16Z | |
| dc.date.issued | 2014-07-13 | |
| dc.description | The 44th International Conference on Environmental Systems was held in Tuscon, Arizona, USA on 13 July 2014 through 17 July 2014. | |
| dc.description | Jeffrey S. Pilgrim, Vista Photonics, Inc, USA | |
| dc.description | William R. Wood, Vista Photonics, Inc, USA | |
| dc.description | Miguel. E. Casias, Vista Photonics, Inc, USA | |
| dc.description | Andrei B. Vakhtin,Vista Photonics, Inc, USA | |
| dc.description | Michael D. Johnson, NanoRacks, LLC, USA | |
| dc.description | Paul D. Mudgett, NASA Johnson Space Center, USA | |
| dc.description.abstract | The International Space Station (ISS) employs a suite of portable and permanently located gas monitors to insure crew health and safety. These sensors are tasked with functions ranging from fixed mass spectrometer based major constituents analysis to portable electrochemical sensor based combustion product monitoring. An all optical multi- gas sensor is being developed that can provide the specificity of a mass spectrometer with the portability of an electrochemical cell. The technology, developed under the Small Business Innovation Research program, allows for an architecture that is rugged, compact and low power. A four gas version called the Multi-Gas Monitor was launched to ISS in November 2013 aboard Soyuz and activated in February 2014. The portable instrument is comprised of a major constituents analyzer (water vapor, carbon dioxide, oxygen) and high dynamic range real-time ammonia sensor. All species are sensed inside the same enhanced path length optical cell with a separate vertical cavity surface emitting laser (VCSEL) targeted at each species. The prototype is controlled digitally with a field-programmable gate array/microcontroller architecture. The optical and electronic approaches are designed for scalability and future versions could add three important acid gases and carbon monoxide combustion product gases to the four species already sensed. Results obtained to date from the technology demonstration on ISS are presented and discussed. | en_US |
| dc.format.mimetype | application/pdf | |
| dc.identifier.isbn | 978-0-692-38220-2 | |
| dc.identifier.other | ICES-2014-058 | |
| dc.identifier.uri | http://hdl.handle.net/2346/59621 | |
| dc.language.iso | eng | en_US |
| dc.publisher | 44th International Conference on Environmental Systems | en_US |
| dc.title | Optical Multi-Gas Monitor Technology Demonstration on the International Space Station | en_US |
| dc.type | Presentation | en_US |