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Design of An Improved Miniature Ion Neutral Mass Spectrometer for NASA ApplicationsThe ion optics of NASA's Ion Neutral Mass Spectrometer (INMS) sensor was simulated with three dimensional models of the open source, the quadrupole deflector, the exit lens system and the quadrupole mass analyzer to design more compact models with lower weight. Comparison of calculated transmission with experimental results shows good agreement. Transmission analyses with varying geometrical parameters and voltages throw light on possible ways of reducing the size of the sensor. Trajectories of ions of mass 1-99 amu were simulated to analyze and optimize transmission. Analysis of open source transmission with varying angle of attack shows that the angular acceptance can be considerably increased by programming the voltages on the ion trap/ collimator. Analysis of transmission sensitivity to voltages and misalignments of the quadrupole deflector rods indicate that increased transmission is possible with a geometrically asymmetrical deflector and a deflector can be designed with much lower sensitivities of transmission. Bringing the disks closer together can decrease the size of the quadrupole deflector and also increase transmission. The exit lens system can be redesigned to be smaller by eliminating at least one electrode entirely without loss of transmission. Ceramic materials were investigated to find suitable candidates for use in the construction of lighter weight mass spectrometer. A high-sensitivity, high-resolution portable gas chromatograph mass spectrometer with a mass range of 2-700 amu has been built and will be commercialized in Phase 3.
Document ID
19970026005
Acquisition Source
Goddard Space Flight Center
Document Type
Contractor Report (CR)
Authors
Swaminathan, Viji K.
(Princeton Electronic Systems, Inc. Princeton, NJ United States)
Alig, Roger C.
(Princeton Electronic Systems, Inc. Princeton, NJ United States)
Date Acquired
September 6, 2013
Publication Date
July 11, 1997
Subject Category
Optics
Report/Patent Number
NASA-CR-204987
PES/NASA-95-1
NASA 1.26:204987
Accession Number
97N25373
Funding Number(s)
CONTRACT_GRANT: NAS5-32823
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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