N-II
From Spacefaring
The N-II or N-2 was a derivative of the American Delta rocket, produced under licence in Japan. It replaced the N-I-rocket in Japanese use. It used a Thor-ELT first stage, a Delta-F|isp}}ond 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.
Wikimedia, Wikidata
N-2
height 35 metre, diameter 2.44 metre, mass 132690 kilogram, payload mass 2000 kilogram, payload mass 730 kilogram,
McDonnell Douglas, Mitsubishi Heavy Industries,
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Japan, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, launch vehicle,
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Location: KML, Cluster Map, Maps,
Tanegashima Space Center
N-II-Rocket-ScaleModel-ISAS-CommHall
Rockets of NASDAandJAXA scalemodels-atJAXATsukubaSpaceDome20250607| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Tanegashima Space Center | Commons | ||
| commons | image | N-II-Rocket-ScaleModel-ISAS-CommHall | Commons | ||
| commons | image | Rockets of NASDAandJAXA scalemodels-atJAXATsukubaSpaceDome20250607 | Commons | ||
