日本地球惑星科学連合2024年大会

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[J] ポスター発表

セッション記号 P (宇宙惑星科学) » P-PS 惑星科学

[P-PS09] 月の科学と探査

2024年5月27日(月) 17:15 〜 18:45 ポスター会場 (幕張メッセ国際展示場 6ホール)

コンビーナ:西野 真木(宇宙航空研究開発機構宇宙科学研究所)、鹿山 雅裕(東京大学大学院総合文化研究科広域科学専攻広域システム科学系)、仲内 悠祐(立命館大学)、小野寺 圭祐(東京大学地震研究所)


17:15 〜 18:45

[PPS09-P02] SLIM搭載マルチバンド分光カメラ(MBC)の着陸後較正

*仲内 悠祐1佐伯 和人1大竹 真紀子2西野 真木3長岡 央1石原 吉明3、佐藤 広幸3本田 親寿2宮崎 理紗3梶谷 伊織3、坂井 真一郎3 (1.立命館大学、2.会津大学、3.宇宙航空研究開発機構)

キーワード:SLIM、MBC、月、月探査

SLIM spacecraft was launched from Tanegashima Space Center in September 7th by JAXA. At January 20th 0:20 (JST), furthermore, SLIM successfully did “pinpoint landing” on the lunar surface. The landing location was 50 m away from the planned location. After landing, we observed some boulders, which might be eject from SHIOLI crater, using Multi-Band Camera (MBC). MBC is a compact VIS-NIR camera composed of an imaging sensor (Vis-InGaAs), a filter-wheel with 10 band-pass filters, a telephoto focusable optical system, and a movable mirror for panning and tilting. The sensor has sensitivity at wavelength from 700 to 1700 nm, which covers the characteristic absorption bands of lunar minerals, especially focused on olivine’s band position around 1000 nm.
We observed the earth, lunar and deep space data from orbit to obtain optical calibration data using MBC. Before landing on the Moon, since a movable mirror, a filter-wheel and a telephoto focusable optical system are locked, the observed wavelength was only 750 nm. The earth observation was carried out on September 22nd over the Arabian Peninsula. The observational area of MBC was the terminator line between day and night. The altitude was ~100,000 km, and spatial resolution was ~10 km/pixel. The lunar observations were carried out on December 30th and January 4th. The observational area of MBC was (297.73E, -75.74N) and (217.71E, -73.67N), respectively. The altitude was 2500-3,600 km, and spatial resolution was ~500 m/pixel. The MBC’s exposure time, which is estimated using lunar radiance and preflight data, was 128 msec on both days. When we observe lunar surface from orbit, the Auto-Exposure function onboard MBC suggested the same exposure time as our estimation (128 msec), and we confirmed that the AE function worked. The dark level obtained preflight calibration and the earth orbit phase shows the good linearity in the range from 15 to 40 degrees of celsius.
After landing, the critical operation of MBC was done perfectly. The three launch locks were smoothly unlocked, and the functions of Auto-Exposure and Auto-Focus were worked. Then, we observed lunar surface regolith, boulders and deep space and obtained 10 band spectral data. Now, we perform calibration using the data of preflight, inflight and after landing.

Acknowledgments: This study is supported by JAXA Lunar and Planetary Exploration Data Analysis group (JLPEDA / JAXA).