ANITA2 Flight Model Development – First ground test results of the Trace Gas Analyser for the ISS (and beyond)

dc.creatorStuffler, Timo
dc.creatorStettner, Armin
dc.creatorSeurig, Roland
dc.creatorGisi, Michael
dc.creatorHonne, Atle
dc.creatorKaspersen, Kristin
dc.creatorBakke, Kari
dc.creatorThielemann, Jens
dc.creatorLiverud, Anders
dc.creatorWitt, Johannes
dc.creatorHovland, Scott
dc.creatorLaurini, Daniele
dc.creatorRebeyre, Pierre
dc.date.accessioned2018-07-06T22:33:35Z
dc.date.available2018-07-06T22:33:35Z
dc.date.issued2018-07-08
dc.descriptionTimo Stuffler, OHB System AG
dc.descriptionAtle Honne, SINTEF
dc.descriptionJohannes Witt, ESA
dc.descriptionArmin Stettner, OHB System AG
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.abstractANITA2 (Analysing Interferometer for Ambient Air) follows the European precursor mission ANITA1, which delivered information on the air conditions analysing in parallel 33 of the most important trace gases on-board ISS in the cabin atmosphere in 2007 and 2008. The data have shown the benefits of in-situ measurements in a manned space cabin atmosphere. The advantages of the ANITA type instruments include high sensitivity, accuracy, precision and time resolution of the measurement data. The gas analyser relies on optical analyses with a Fourier Transform Infrared spectrometer. In 2016, OHB System and SINTEF were awarded by ESA the contract to develop the ANITA2 flight model. The new system is characterised by a major reduction in mass, volume and power consumption, as well as improved characteristics in gas analysis sensitivity. The novel, sophisticated analysis SW is further improved, employing statistical and non-linear calibration and analysis methods. As for ANITA1, the programme is planned to be a joint ESA/NASA project. It is also a stepping stone into the future, as a precursor system for manned exploration missions, e.g. to Mars and the Moon. The paper presents the newly developed and built optomechanical components of the new ANITA2 instrument. It also presents the fully operating optical BB, featuring flight-light build components, and includes the first measurement results. The work described is performed under contract of the European Space Agency ESA.en_US
dc.identifier.otherICES_2018_67
dc.identifier.urihttp://hdl.handle.net/2346/74073
dc.language.isoengen_US
dc.publisher48th International Conference on Environmental Systemsen_US
dc.subjectISS air monitoring
dc.subjectquasi on-line air analyses
dc.subjectFTIR interferometer
dc.subjectlong-term development programme
dc.titleANITA2 Flight Model Development – First ground test results of the Trace Gas Analyser for the ISS (and beyond)en_US
dc.typePresentationen_US

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