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1.
J Am Soc Mass Spectrom ; 19(10): 1411-8, 2008 Oct.
Article in English | MEDLINE | ID: mdl-18620866

ABSTRACT

The visualization of hazardous gaseous emissions at volcanoes using in-situ mass spectrometry (MS) is a key step towards a better comprehension of the geophysical phenomena surrounding eruptive activity. In-situ data consisting of helium, carbon dioxide, sulfur dioxide, and other gas species, were acquired with a quadrupole based MS system. Global position systems (GPS) and MS data were plotted on ground imagery, topography, and remote sensing data collected by a host of instruments during the second Costa Rica Airborne Research and Technology Applications (CARTA) mission. This combination of gas and imaging data allowed three-dimensional (3D) visualization of the volcanic plume and the mapping of gas concentration at several volcanic structures and urban areas. This combined set of data has demonstrated a better tool to assess hazardous conditions by visualizing and modeling of possible scenarios of volcanic activity. The MS system is used for in-situ measurement of 3D gas concentrations at different volcanic locations with three different transportation platforms: aircraft, auto, and hand-carried. The demonstration for urban contamination mapping is also presented as another possible use for the MS system.


Subject(s)
Gases/analysis , Mass Spectrometry/instrumentation , Mass Spectrometry/methods , Volcanic Eruptions/analysis , Air Pollution/analysis , Aircraft , Automobiles , Carbon Dioxide/analysis , Costa Rica , Sulfur Dioxide/analysis , Water/analysis
2.
J Am Soc Mass Spectrom ; 13(9): 1120-8, 2002 Sep.
Article in English | MEDLINE | ID: mdl-12322959

ABSTRACT

The use of a quadrupole ion trap mass spectrometer (QITMS) for quantitative analysis of hydrogen and helium as well as of other permanent gases is demonstrated. Like commercial instruments, the customized QITMS uses mass selective instability; however, this instrument operates at a greater trapping frequency and without a buffer gas. Thus, a useable mass range from 2 to over 50 daltons (Da) is achieved. The performance of the ion trap is evaluated using part-per-million (ppm) concentrations of hydrogen, helium, oxygen, and argon mixed into a nitrogen gas stream, as outlined by the National Aeronautics and Space Administration (NASA), which is interested in monitoring for cryogenic fuel leaks within the Space Shuttle during launch preparations. When quantitating the four analytes, relative accuracy and precision were better than the NASA-required minimum of 10% error and 5% deviation, respectively. Limits of detection were below the NASA requirement of 25-ppm hydrogen and 100-ppm helium; those for oxygen and argon were within the same order of magnitude as the requirements. These results were achieved at a fast data recording rate, and demonstrate the utility of the QITMS as a real-time quantitative monitoring device for permanent gas analysis.


Subject(s)
Argon/analysis , Environmental Monitoring/methods , Helium/analysis , Hydrogen/analysis , Mass Spectrometry/methods , Oxygen/analysis , Environmental Monitoring/instrumentation , Environmental Monitoring/standards , Evaluation Studies as Topic , Hazardous Substances/analysis , Hazardous Substances/standards , Ions , Mass Spectrometry/instrumentation , Mass Spectrometry/standards , Nitrogen , Spacecraft/instrumentation , Spacecraft/standards , United States , United States National Aeronautics and Space Administration/standards
3.
J Am Soc Mass Spectrom ; 13(8): 1004-12, 2002 Aug.
Article in English | MEDLINE | ID: mdl-12216728

ABSTRACT

This work is aimed at understanding the aspects of designing a miniature mass spectrometer (MS) system. Several types of small MS systems are evaluated and discussed, including linear quadrupole, quadrupole ion trap, time of flight, and sector. Analysis of hydrogen, helium, oxygen, and argon in a nitrogen background with the concentrations of the components of interest ranging from 0 to 5000 parts per million (ppm). The performance of each system in terms of accuracy, precision, limits of detection, response time, recovery time, scan rate, size, and weight is assessed. The relative accuracies of the systems varied from <1% to approximately 40% with an average below 10%. Relative precisions varied from 1% to 20%, with an average below 5%. The detection limits had a large distribution, ranging from 0.2 to 170 ppm. The systems had a diverse response time ranging from 4 to 210 s, as did the recovery time with a 6-to-210-s distribution. Most instruments had scan times near 1 s; however, one instrument exceeded 13 s. System weights varied from 9 to 52 kg and sizes ranged from 15 x 10(3) cm3 to 110 x 10(3) cm3. A performance scale is set up to rank each system, and an overall performance score is given to each system.

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