Q3130574

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.

MainWikipediaGalleryBibliographyTableSearch

Wikimedia, Wikidata
N-2
height 35 metre, diameter 2.44 metre, mass 132690 kilogram, payload mass 2000 kilogram, payload mass 730 kilogram, 
launch vehicle, 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, Tarshish, Dong Fang Hong 2, Ekran, launch vehicle, Republic of Haiti, 

​

Location: KML, Cluster Map, Maps,

Frameless

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