日本地球惑星科学連合2022年大会

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[J] 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-PS06] 月の科学と探査

2022年5月27日(金) 15:30 〜 17:00 301B (幕張メッセ国際会議場)

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)、コンビーナ: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)、長岡 央(理化学研究所)、コンビーナ:仲内 悠祐(宇宙航空研究開発機構)、座長:仲内 悠祐(宇宙航空研究開発機構)、西野 真木(宇宙航空研究開発機構宇宙科学研究所)

16:30 〜 16:45

[PPS06-17] SLIM着陸機搭載マルチバンドカメラMBCの開発完了報告

*佐伯 和人1仲内 悠祐2大竹 真紀子3、佐藤 広幸2石原 吉明2長岡 央4本田 親寿3白石 浩章2山中 千博1、前田 孝雄5西谷 隆介3荒木 亮太郎1加藤 礼也1、坂井 真一郎2、澤井 秀次郎2、福田 盛介2、櫛木 賢一2 (1.大阪大学、2.宇宙航空研究開発機構、3.会津大学、4.理化学研究所、5.東京農工大学)

キーワード:月、近赤外分光法、かんらん石

Smart Lander for Investigating Moon (SLIM) project promoted by JAXA is in the final stage. It will be launched in fiscal year 2022 as JAXA's first lunar-soft-landing mission. The main purpose of this project is to demonstrate various techniques for pinpoint landing within a hundred meters in radius on the moon. Demonstration of the SLIM landing technology will cause a paradigm shift from "exploring where it is easy to land" to "exploring where we want to land". After landing, the SLIM project plans to operate Multi-Band Camera (MBC) to observe around the landing site. We have just finished testing the flight model of MBC and completed the development.
As a landing site for SLIM mission, one of the small fresh craters just outside of the Theophilus crater is selected. This crater (diameter ~200 m) locates 13.3oS, 25.2oE outside the southwest rim of Theophilus and named "Shioli". There is olivine-rich lithology, which is probably mantle (or the lower part of the crustal) origin excavated by the Nectaris basin forming impact as suggested by the global distribution of the olivine-rich sites (Yamamoto et al. , 2010) , well before the formation of the Theophilus.
In order to identify this unknown lithology and estimate its origin, MBC has a spatial resolution (1.3 mm/pixel at 10 m) that distinguishes plutonic rock texture and a band combination (10 bands; 750, 920, 950, 970, 1000, 1050, 1100, 1250, 1550, 1650 (nm)) that identifies mineral species and estimates Mg#(=Mg/(Mg+Fe) atomic ratio) of olivine.
MBC passed various functional performance tests and environmental tests and was delivered to JAXA. Some specifications were relaxed during developing phase. The final performance of MBC and the optimized operation procedure will be explained.