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  • The First Japan’s Planetary Orbiter AKATSUKI and its Scientific Results

    Paper number

    IAC-16,A3,5,1,x33129

    Coauthor

    Prof. Masato Nakamura, ISAS/JAXA, Japan

    Coauthor

    Prof. Nobuaki Ishii, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Dr. Takeshi Imamura, ISAS/JAXA, Japan

    Coauthor

    Ms. Chikako Hirose, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Dr. Atsushi Yamazaki, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Mr. Junichi Nakatsuka, Japan

    Coauthor

    Dr. Tsutomu Ichikawa, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Dr. Tomoaki Toda, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Dr. Hiroyuki Toyota, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Mr. Sumitaka Tachikawa, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Prof. Yukio Kamata, Institute of Space and Astronautical Science, Japan

    Coauthor

    Prof. Naomoto Iwagami, Japan

    Coauthor

    Dr. Takehiko Satoh, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Prof. Makoto Taguchi, Japan

    Coauthor

    Prof. Shigeto Watanabe, Hokkaido University, Japan

    Coauthor

    Prof. Yukihiro Takahashi, Hokkaido University, Japan

    Coauthor

    Dr. Makoto Suzuki, Japan

    Coauthor

    Prof. Munetala Ueno, Japan

    Coauthor

    Prof. Takumi Abe, Japan

    Coauthor

    Dr. Takao M. Sato, Japan

    Coauthor

    Dr. Shin-ya Murakami, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Dr. Yukio Yamamoto, ISAS/JAXA, Japan

    Coauthor

    Dr. Tetsuya Fukuhara, Japan

    Coauthor

    Dr. Manabu Yamada, Japan

    Coauthor

    Dr. George L. Hashimoto, Japan

    Coauthor

    Dr. Naru Hiram, Japan

    Coauthor

    Dr. Toru Kouyama, National Institute of Advanced Industrial Science of Technology (AIST), Japan

    Coauthor

    Dr. Hiroki Ando, Japan

    Coauthor

    Dr. Ko-ichiro Sugiyama, Japan

    Coauthor

    Dr. Hiroki Kashimura, JAMSTEC, Japan

    Coauthor

    Prof. Shoko Ohtsuki, Japan

    Coauthor

    Dr. Kazunori Ogohara, Japan

    Year

    2016

    Abstract
    Japan’s Venus Climate Orbiter Akatsuki was proposed to ISAS (Institute of Space and Astronautical Science) in 2001 as an interplanetary mission. We made 5 cameras with narrow-band filters to image Venus at different wavelengths to track the cloud and minor components distribution at different heights to study the Venusian atmospheric dynamics in 3 dimension. 
    
    It was launched on May 21st, 2010 and reached Venus on December 7th, 2010. With the thrust by the orbital maneuver engine, Akatsuki tried to go into the westward equatorial orbit around Venus with the 30 hours’ orbital period, however it failed by the malfunction of the propulsion system. Later the spacecraft has been orbiting the sun for 5 years. On December 7th, 2015 Akatsuki met Venus again after the orbit control and Akatsuki was put into the westward equatorial orbit whose apoapsis is about 0.44 million km and orbital period of 14 days.
    
    Its main target is to shed light on the mechanism of the fast atmospheric circulation of Venus. The systematic imaging sequence by Akatsuki is advantageous for detecting meteorological phenomena with various temporal and spatial scales. We have five photometric sensors as mission instruments for imaging, which are 1 μm-infrared camera (IR1), 2 μm- infrared camera (IR2), ultra-violet imager (UVI), long-wave infrared camera (LIR), and lightning and airglow camera (LAC). These photometers except LIR have changeable filters in the optics to image in certain wavelengths. Akatsuki’s long elliptical orbit around Venus is suitable for obtaining cloud-tracked wind vectors over a wide area continuously from high altitudes. With the observation, the characterizations of the meridional circulation, mid-latitude jets, and various wave activities are anticipated. 
    
    The technical issues of Venus orbit insertion in 2015 and the scientific new results will be given in this paper.
    Abstract document

    IAC-16,A3,5,1,x33129.brief.pdf

    Manuscript document

    IAC-16,A3,5,1,x33129.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.