著者

森 大吉郎 小野田 淳次郎 橋元 保雄 村上 卓司 白銀 博 小野島 昇

出版者

東京大学宇宙航空研究所

雑誌

東京大学宇宙航空研究所報告 (ISSN:05638100)

巻号頁・発行日

vol.16, no.4, pp.p1207-1221, 1980-11

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資料番号: SA0125912000

著者

橋元 保雄 中田 篤 市田 和夫 池田 光之 平山 昇司 平田 安弘

出版者

宇宙航空研究開発機構

雑誌

宇宙科学研究所報告. 特集 (ISSN:02859920)

巻号頁・発行日

vol.16, pp.405-418, 1986-10

著者

森 大吉郎 橋元 保雄 中田 篤 上杉 国憲 西田 稔夫 福沢 清

出版者

宇宙航空研究開発機構

雑誌

宇宙科学研究所報告 (ISSN:02852853)

巻号頁・発行日

vol.17, pp.1-69, 1984-02

被引用文献数

1

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Mu rocket assembly and launch system was renewed on the same place where the former one had stood on. After breaking down of the former one, the foundation work started on April 1981,and all of the construction finished on August 1982. This system consists of a rocket assembly tower and a launcher. The assembly tower is a steel-framed truss structure building which has 11 floors and contains cranes, big doors, and movable floors necessary to bring in, assemble, and check out the Mu rocket. This tower is 43m high, 18m wide, 13m deep, and 700 ton in weight. The launcher is 300 ton in weight and made up of a boom structure and guide rails on which a rocket slides away. This launcher can revolve by bogies on a circular rail from the assembly tower toward the launching point. A flame deflector cooled by water is automatically installed to the launcher during its revolution. On February 20 1983,M-3S-3 rocket was successfully launced as the first satellite launch using this system.