Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft

The main requirements imposed upon ion sources for on-board time-of-flight mass spectrometers are considered in the paper. An approximate formula to calculate the ionization cross section of an analyte substance is given. The dependence of the probability of analyte ionization for the selected ion s...

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Main Authors: N. D. Semkin, I. V. Piyakov, M. A. Rodina, D. V. Rodin
Format: Article
Language:English
Published: Samara National Research University 2016-12-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/3127/3037
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spelling doaj-07de3d9079dc4fa5b13834feff7a7d202021-08-25T09:12:04ZengSamara National Research UniversityВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение2542-04532541-75332016-12-0115319720310.18287/2541-7533-2016-15-3-197-2032917Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraftN. D. Semkin0I. V. Piyakov1M. A. Rodina2D. V. Rodin3Samara National Research UniversitySamara National Research UniversitySamara National Research UniversitySamara National Research UniversityThe main requirements imposed upon ion sources for on-board time-of-flight mass spectrometers are considered in the paper. An approximate formula to calculate the ionization cross section of an analyte substance is given. The dependence of the probability of analyte ionization for the selected ion source design is shown. Several deigns of ion sources are proposed that provide the required width of the zone of ionization by selecting source parameters. A design of the ion source providing increased reliability and lifetime of the unit is selected for the use in scientific equipment DMS-01 installed aboard small spacecraft AIST number 2. The results of a laboratory experiment on the operation of this design of the source are presented. The data obtained confirm the applicability of the Lotz-Drevins approximation formula to determine the probability of ionization of atoms or molecules of an analyte in the chosen design of the ion source.https://journals.ssau.ru/vestnik/article/viewFile/3127/3037ion sourcetime-of-flight mass spectrometeron-board mass spectrometersmall spacecraftapproximation formulareliabilityconstructionionization probability
collection DOAJ
language English
format Article
sources DOAJ
author N. D. Semkin
I. V. Piyakov
M. A. Rodina
D. V. Rodin
spellingShingle N. D. Semkin
I. V. Piyakov
M. A. Rodina
D. V. Rodin
Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
ion source
time-of-flight mass spectrometer
on-board mass spectrometer
small spacecraft
approximation formula
reliability
construction
ionization probability
author_facet N. D. Semkin
I. V. Piyakov
M. A. Rodina
D. V. Rodin
author_sort N. D. Semkin
title Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft
title_short Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft
title_full Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft
title_fullStr Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft
title_full_unstemmed Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft
title_sort ion source of dms-01 scientific equipment for «aist no 2» small spacecraft
publisher Samara National Research University
series Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
issn 2542-0453
2541-7533
publishDate 2016-12-01
description The main requirements imposed upon ion sources for on-board time-of-flight mass spectrometers are considered in the paper. An approximate formula to calculate the ionization cross section of an analyte substance is given. The dependence of the probability of analyte ionization for the selected ion source design is shown. Several deigns of ion sources are proposed that provide the required width of the zone of ionization by selecting source parameters. A design of the ion source providing increased reliability and lifetime of the unit is selected for the use in scientific equipment DMS-01 installed aboard small spacecraft AIST number 2. The results of a laboratory experiment on the operation of this design of the source are presented. The data obtained confirm the applicability of the Lotz-Drevins approximation formula to determine the probability of ionization of atoms or molecules of an analyte in the chosen design of the ion source.
topic ion source
time-of-flight mass spectrometer
on-board mass spectrometer
small spacecraft
approximation formula
reliability
construction
ionization probability
url https://journals.ssau.ru/vestnik/article/viewFile/3127/3037
work_keys_str_mv AT ndsemkin ionsourceofdms01scientificequipmentforaistno2smallspacecraft
AT ivpiyakov ionsourceofdms01scientificequipmentforaistno2smallspacecraft
AT marodina ionsourceofdms01scientificequipmentforaistno2smallspacecraft
AT dvrodin ionsourceofdms01scientificequipmentforaistno2smallspacecraft
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