日本地球惑星科学連合2021年大会

講演情報

[E] ポスター発表

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-CG17] 宇宙・惑星探査の将来計画および関連する機器開発の展望

2021年6月4日(金) 17:15 〜 18:30 Ch.06

コンビーナ:小川 和律(宇宙航空研究開発機構)、尾崎 光紀(金沢大学理工研究域電子情報学系)、坂谷 尚哉(立教大学 理学部 物理学科)、吉岡 和夫(東京大学大学院新領域創成科学研究科)

17:15 〜 18:30

[PCG17-P14] Observation Plans and Development Status of MIRS: MMX Infrared Spectrometer on the MMX Spacecraft

*岩田 隆浩1、中川 広務2、土屋 史紀2、中村 智樹2、Barucci Maria Antonietta3、Reess Jean-Michel3、Bernardi Pernelle3、Doressoundiram Alain3、Fornasier Sonia3、Le Du Michel4、Sawyer Eric4 (1.宇宙航空研究開発機構 宇宙科学研究所、2.東北大学、3.パリ天文台 LESIA、4.CNES)

キーワード:MMX、フォボス、デイモス、赤外線分光計、含水鉱物、火星大気

The Martian Moons Exploration (MMX) is a probe which will be launched by the Japanese launch vehicle H-III, and it will navigate the quasi satellite orbit of Phobos and will make a fly-by of Deimos. MIRS (MMX InfraRed Spectrometer) is a push-broom imaging spectrometer in the wavelength range of 0.9 to 3.6 micrometers which is one of the candidate instruments to be installed on the MMX spacecraft. It has a field-of-view (FOV) of 3.3 deg width with instantaneous-FOV (IFOV) of 0.35 mrad, which can be scanned by inner along track scan mirror in the range of ±20 deg.
MMX aims to elucidate the evolution of our solar system by investigating the migration process of primitive bodies in the early stage. MIRS will observe absorptions of hydroxide or hydrated minerals on Phobos and Deimos in the wavelength range of 2.7-3.2 micrometers. By analyzing the behavior of the spectra, we will distinguish between structural water in hydrous silicate minerals, and water ice particles. MIRS will also try to detect the absorption of organic matters in the wavelength range of 3.3-3.5 micrometers. These results will be crucial evidence to answer the question of the origin of the Martian satellites and identify whether they are satellites formed by a giant impact or primitive asteroids captured by Mars gravitational field. MIRS will observe Phobos to survey the sampling site candidates, to investigate the sampling site precisely at the touch-down mode, and to make global mapping. The global mapping of Phobos to select prior areas and landing sites will be performed on the quasi satellite orbit. Precise mapping for candidate landing sites will be followed on the lower altitude. Observations for Deimos will be basically executed from the fly-by orbit. MIRS will also monitor the Martian atmosphere with particular attention to spatial and temporal changes as clouds, dust and water vapor. We will report and discuss on the observation plans and the development status of the MIRS instrument.