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Development of the Third Generation JPL Electronic Nose for International Space Station Technology Demonstration
Author(s) -
Abhijit V. Shevade,
M. L. Homer,
Hanying Zhou,
April D. Jewell,
Adam Kisor,
K. Manatt,
Julia Torres,
Jordi Soler Soler,
Shiao -Pin S. Yen,
M. A. Ryan,
Mario Blanco,
William A. Goddard
Publication year - 2007
Publication title -
sae technical papers on cd-rom/sae technical paper series
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.295
H-Index - 107
eISSN - 1083-4958
pISSN - 0148-7191
DOI - 10.4271/2007-01-3149
Subject(s) - space technology , space (punctuation) , international space station , aerospace engineering , computer science , electrical engineering , systems engineering , engineering , aeronautics , operating system
The capabilities of the JPL Electronic Nose have been expanded to include characteristics required for a Technology Demonstration schedule on the International Space Station (ISS) in 2008-2009 (1,2). Concurrently, to accommodate specific needs on ISS, the processes, tools and analyses which influence all aspects of development of the device have also been expanded. The Third Generation ENose developed for this program uses two types of sensor substrates, newly developed inorganic and organic sensor materials, redesigned electronics, onboard near real-time data analysis and power and data interfaces specifically for ISS. This paper will discuss the Third Generation ENose with a focus on detection of mercury in the parts-per-billion range.

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