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・ N-Gage (service)
・ N-Gage QD
・ N-Glycolylneuraminic acid
・ N-gram
・ N-group
・ N-group (category theory)
・ N-group (finite group theory)
・ N-gumla
・ N-Hash
・ N-hydroxy-2-acetamidofluorene reductase
・ N-hydroxyarylamine O-acetyltransferase
・ N-Hydroxypiperidine
・ N-Hydroxysuccinimide
・ N-hydroxythioamide S-beta-glucosyltransferase
・ N-I (rocket)
N-II (rocket)
・ N-isopropylammelide isopropylaminohydrolase
・ N-jet
・ N-Joi
・ N-JOY
・ N-Joy
・ N-Joypad
・ N-linked glycosylation
・ N-localizer
・ N-malonylurea hydrolase
・ N-methyl nucleosidase
・ N-methyl-2-oxoglutaramate hydrolase
・ N-Methyl-2-pyrrolidone
・ N-Methyl-3-piperidyl benzilate
・ N-Methyl-D-aspartic acid


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N-II (rocket) : ウィキペディア英語版
N-II (rocket)

|family = Delta
|status = Retired
|sites = LA-N, Tanegashima
|launches = 8
|success = 8
|first = 11 February 1981
|last = 19 February 1987
|stagedata =
}}
The N-II or N-2 was a derivative of the American Delta rocket, produced under licence in Japan. It used a Thor-ELT first stage, a Delta-F second stage, nine Castor SRMs, and on most flights either a Star-37E or Burner-2 upper stage, identical to the US Delta 0100 series configurations. Eight were launched between 1981 and 1987, before it was replaced by the H-I, which featured Japanese-produced upper stages. All eight launches were successful.
==Launch history==


抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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