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・ H-cobordism
・ H-Craft Championship
・ H-dagurinn
・ H-derivative
・ H-Dhami
・ H-drive
・ H-dropping
・ H-E Double Hockey Sticks
・ H-E-B
・ H-E-B Mexico
・ H-Eugene
・ H-factor
・ H-G-W Partners
・ H-Gun
・ H-hour (D-day)
H-I
・ H-II
・ H-II Transfer Vehicle
・ H-IIA
・ H-IIB
・ H-index
・ H-infinity loop-shaping
・ H-infinity methods in control theory
・ H-Invitational
・ H-L-V School District
・ H-Logic
・ H-Net
・ H-P Products
・ H-point
・ H-Prize


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H-I : ウィキペディア英語版
H-I

|family = Thor
|comparable = Delta
|status = Retired
|sites = LA-N, Tanegashima
|launches = 9
|success = 9
|first = 12 August 1986
|last = 11 February 1992
|stagedata =
}}
The H-I or H-1 was a Japanese liquid-fuelled carrier rocket, consisting of a licence-produced American first stage and set of booster rockets, and all-Japanese upper stages. It was launched nine times between 1986 and 1992. It replaced the N-II, and was subsequently replaced by the H-II, which used the same upper stages with a Japanese first stage.
The first stage of the H-I was a licence-built version of the Thor-ELT, which was originally constructed for the US Delta 1000 rocket. The stage had already been licence produced in Japan for the N-I and N-II rockets. The second stage was entirely Japanese, using an LE-5 engine. On launches to Geosynchronous transfer orbits, a Nissan-produced UM-129A solid motor was used as a third stage. Depending on the mass of the payload, either six or nine US Castor 2 SRMs would be used as booster rockets.
==Launch history==


抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「H-I」の詳細全文を読む



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