日本地球惑星科学連合2015年大会

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セッション記号 P (宇宙惑星科学) » P-CG 宇宙惑星科学複合領域・一般

[P-CG31] 宇宙科学・探査の将来計画と関連する機器・技術の現状と展望

2015年5月28日(木) 16:15 〜 18:00 202 (2F)

コンビーナ:*平原 聖文(名古屋大学太陽地球環境研究所)、小嶋 浩嗣(京都大学生存圏研究所)、高橋 幸弘(北海道大学・大学院理学院・宇宙理学専攻)、鈴木 睦(宇宙航空研究開発機構宇宙科学研究本部)、座長:小嶋 浩嗣(京都大学生存圏研究所)、高橋 幸弘(北海道大学・大学院理学院・宇宙理学専攻)

16:15 〜 16:30

[PCG31-17] 超熱的イオン質量分析器(STIMS)の設計

*石黒 恵介1平原 聖文1 (1.名古屋大学太陽地球環境研究所)

キーワード:イオン質量分析器, 超熱的イオン, 非磁化惑星, 惑星電離圏

Ion escape processes are critical issues to solve atmospheric evolution of non-magnetized planets, e.g., Venus and Mars. Many studies about the ion escape have been conducted by both observational and theoretical methods. There is, however, a problem that qualities of in-situ observations have not been sufficient to identify the detailed suprathermal plasma dynamics, especially about molecular ions, around the non-magnetized planetary ionospheres. A suprathermal ion mass spectrometer (STIMS) has been designed for future in-situ observations of three dimensional velocity distributions for suprathermal ions around the planetary atmospheres.
The STIMS consists of (a.) an energy analyzer and (b.) a mass analyzer. A field of view of the STIMS is about 4 pi sr per a half spin of spin-stabilized spacecraft. A target energy range is from 0.1 to 300 eV, which corresponds to suprathermal energies, and a mass range is from 1 to 50 amu. An energy resolution, ∆E/E, is less than 5%, and a mass resolution, M/∆M, is over 10.
(a.) An energy analysis of the STIMS is carried out in a top-hat type electrostatic analyzer, which deflects incident ions by 90 degrees and leads them to an entrance of the mass analyzer. Only ions that fly along a center radius of spherical electrodes are able to get to the mass analyzer.
(b.) The mass analyzer of the STIMS is mainly made up of a pre-acceleration section and a magnet section. The magnet section, which has a cylindrically symmetric structure, is divided into sixteen regions by permanent sector magnets. Firstly, in the pre-acceleration section, ions which got through the energy analyzer are accelerated or decelerated by an acceleration voltage E eV, whose magnitudes depend on mass number of the ions M amu. Secondly, the accelerated/decelerated ions experience Lorentz force in the magnet section, and reach a micro-channel plate (MCP), with semicircular trajectories. By sweeping magnitudes of the acceleration voltage E, only ions that conserve square root of product of their masses and kinetic energies, i.e., √ME, are able to reach the MCP.
As for observations of molecular ions, magnet type mass spectrometers have a great advantage that it is possible to detect the molecular ions without dissociations. However, this type of spectrometer has several disadvantages; (1) it is difficult to discriminate between noise signals and ion signals at the MCP because this type of spectrometer does not take signal coincidences; (2) this type of mass spectrometer tends to be heavier than other types of spectrometers due to installing magnets; (3) magnetic field of the magnets might cause undesirable effect on other observation instruments on spacecraft.
In this presentation, we will introduce design concepts and specifications of the STIMS.