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  • CURRENT STATUS AND EVOLVING PLAN OF JAPANESE FLAGSHIP LAUNCH SYSTEM, H-IIA/H-IIB and H3

    Paper number

    IAC-16,D2,1,4,x32298

    Coauthor

    Mr. Akihiro Sato, Mitsubishi Heavy Industries, Ltd., Japan

    Coauthor

    Mr. Takashi Noma, Mitsubishi Heavy Industries, Ltd., Japan

    Coauthor

    Mr. Mayuki Niitsu, Mitsubishi Heavy Industries Ltd. - Nagoya Aerospace Systems, Japan

    Coauthor

    Mr. Tatsuru Tokunaga, Mitsubishi Heavy Industries, Ltd., Japan

    Coauthor

    Mr. Tokio Nara, Mitsubishi Heavy Industries, Ltd., Japan

    Coauthor

    Mr. Shintaro Nishihira, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Mr. Makoto Arita, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Mr. Masashi Okada, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Mr. Michio Kawakami, Japan Aerospace Exploration Agency (JAXA), Japan

    Year

    2016

    Abstract
    The Japanese flagship launcher, H-IIA and H-IIB have succeeded continuously and the launch success rate has reached to 97.1 percent. Last year, the H-IIA flight No. 29 launched a commercial satellite in Nov. 2015. Some new technologies developed by Japan Aerospace Exploration Agency (JAXA) were adopted in the flight, so that the upgraded H-IIA is able to inject satellites closer to geostationary orbit than conventional geostationary transfer orbit. To meet various commercial satellite needs, the “upgrade” could enhance its performance with some optional items. Therefore, the Japanese government started developing a new flagship launch vehicle, the H3, in order to be more competitive in the satellite launch market. The first launch of the H3 is planned for FY2020. The launcher would provide an attractive price, almost half the price compared with the current launcher such as H-IIA and H-IIB, and high reliability succeeding from the current launchers. Some of the development tests were started performing on avionics, structure and propulsion system. The current status of the H3 development is reported in this paper.
    Abstract document

    IAC-16,D2,1,4,x32298.brief.pdf

    Manuscript document

    IAC-16,D2,1,4,x32298.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.