日本地球惑星科学連合2024年大会

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[E] 口頭発表

セッション記号 P (宇宙惑星科学) » P-PS 惑星科学

[P-PS05] Mercury Science and Exploration

2024年5月31日(金) 13:45 〜 15:15 展示場特設会場 (2) (幕張メッセ国際展示場 6ホール)

コンビーナ:村上 豪(宇宙航空研究開発機構宇宙科学研究所)、相澤 紗絵(Institute de Recherche en Astrophysique et Planetologie)、原田 裕己(京都大学理学研究科)、鎌田 俊一(北海道大学 理学研究院)、座長:鎌田 俊一(北海道大学 理学研究院)、鈴木 雄大(宇宙航空研究開発機構)

14:00 〜 14:15

[PPS05-02] MERTIS - The MErcury Radiometer and Thermal infrared Imaging Spectrometer on its way to Mercury

*Jorn Helbert1、Alessandro Maturilli1、Solmaz Adeli1Oceane Barraud1、Giulia Alemanno1、Mario D'Amore1、Aurelie van Den Neucker1、Nimisha Verma1、Gisbert Peter1、Harald Hiesinger2 (1.German Aerospace Center、2.WWU Münster)

キーワード:Mercury, infrared, terrestrial planets, solar system

MERTIS will map the whole surface of Mercury with a spatial resolution of 500m for the spectrometer channel and 2km for the radiometer channel. The compositional map of Mercury provided by MERTIS will allow unique insights into the evolution of the least explored terrestrial planet. MERTIS will also address directly questions raised by the NASA MESSENGER mission. For example we will be able to provide spatially re-solved compositional information on the hollows and pyroclastic deposits and answer the question whether hollows are actually predominately sulfide deposits.
MERTIS combines a push-broom IR grating spectrometer (TIS) with a radiometer (TIR). TIS operates between 7 and 14 µm and will record dayside radiance spectra of Mercury to infer surface emissivity characteristics, whereas TIR is going to measure the surface temperature (80 -700 K) at night- and dayside in the spectral range from 7-40 µm. TIR is implemented by an in-plane separation arrangement. In this configuration the two radiometer detector lines form the slit of the TIS channel which is an imaging spectrometer. It uses the first European-built space-qualified uncooled microbolometer array. The optical design of MERTIS combines a three mirror anastigmat (TMA) with a modified Offner grating spectrometer. A pointing device allows viewing the planet (planet-baffle), deep space (space-baffle), and two black bodies at 300 K and 700 K temperature, respectively.
MERTIS has successfully obtained observations of the Moon and Venus during flybys. Using the data from the flybys allowed to show that MERTIS shows a performance that significantly exceeds the requirements. The flybys also helped to improve the calibration as well as optimize the operation of the instrument.