期刊论文详细信息
Earth, Planets and Space
Design of telescopic nadir imager for geomorphology (TENGOO) and observation of surface reflectance by optical chromatic imager (OROCHI) for the Martian Moons Exploration (MMX)
Toru Kouyama1  Takaya Okamoto2  Keigo Enya2  Masanobu Ozaki2  Atsushi Yamazaki2  Takahiro Ishimaru2  Takeshi Takashima2  Tsubasa Aoyama3  Yuya Goda3  Satoko Mizumoto3  Hajime Murao3  Saori Fujishima3  Noriko Tanaka3  Keiji Hagiwara3  Hidehiko Suzuki4  Hironobu Sakuta5  Kenji Tanaka5  Kousuke Murakami5  Miho Matsumoto5  Cheng-Ling Kuo6  Ryota Fuse7  Shinsuke Abe7  Peng Hong8  Ko Ishibashi8  Hiroki Kato9  Naoya Osada9  Naoya Sakatani9  Shingo Kameda1,10  Hideaki Miyamoto1,11  Ryoya Ishigami1,12  Tomoki Nakamura1,13 
[1] AIST, Tokyo, Japan;ISAS/JAXA, Tokyo, Japan;MEISEI, Tokyo, Japan;Meiji University, Tokyo, Japan;NIKON, Tokyo, Japan;National Central University, Taoyuan, Taiwan;Nihon University, Chiba, Japan;PERC/Chitech, Chiba, Japan;Rikkyo University, Tokyo, Japan;Rikkyo University, Tokyo, Japan;ISAS/JAXA, Tokyo, Japan;The University of Tokyo, Tokyo, Japan;The Wakasa Wan Energy Research Center, Tsuruga, Japan;Tohoku University, Tokyo, Japan;
关键词: MMX;    TENGOO;    OROCHI;    Imager;    Phobos;    Deimos;    Mars;   
DOI  :  10.1186/s40623-021-01462-9
来源: Springer
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【 摘 要 】

The JAXA’s Martian Moons Exploration (MMX) mission is planned to reveal the origin of Phobos and Deimos. It will remotely observe both moons and return a sample from Phobos. The nominal instruments include the TElescopic Nadir imager for GeOmOrphology (TENGOO) and Optical RadiOmeter composed of CHromatic Imagers (OROCHI). The scientific objective of TENGOO is to obtain the geomorphological features of Phobos and Deimos. The spatial resolution of TENGOO is 0.3 m at an altitude of 25 km in the quasi-satellite orbit. The scientific objective of OROCHI is to obtain material distribution using spectral mapping. OROCHI possesses seven wide-angle bandpass imagers without a filter wheel and one monochromatic imager dedicated to the observation during the landing phase. Using these two instruments, we plan to select landing sites and obtain information that supports the analysis of return samples.Graphical Abstract

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