H-IIB

The H-IIB (H2B) was a Japanese expendable launch system jointly developed by JAXA and Mitsubishi Heavy Industries. It was used exclusively to launch the H-II Transfer Vehicle cargo spacecraft to the International Space Station.

MainWikipediaGalleryBibliographyTableSearchFiles

Wikimedia, Wikidata
H-2B; H2B
diameter 5.2 metre, height 56.6 metre, 
H-II, Mitsubishi Heavy Industries, Japan, 
Kounotori 7, Flight 8, Republic of Haiti, H-II, Dong Fang Hong 2, We-Wish, TechEdSat 3p, Raiko, PicoDragon, Niwaka, Kounotori 9, Kounotori 8, Japan, Kounotori 6, Kounotori 5, Kounotori 4, Kounotori 3, Kounotori 2, HTV-1, F-1, ARDUSAT X, ArduSat 1, AQT-D, 

​

Location: KML, Cluster Map, Maps,

Frameless

Tanegashima Space Center

Mock-up of H-2B rocket

HIIB F NAGOYA S M

HIIB F NAGOYA S M

H-2B Model in Komaki Air Base 20140223

Nagoya City Science Museum 20150125-2

H-IIB Rocket in front of Nagoya City Science Museum 20150125

Nagoya City Science Museum 20150125-1

Panther of the week: Senior Airman Matthew Greger

H-IIB No. F8 on the launch pad

Type	Subtype	Date	Description	Notes	Source
commons	image		Tanegashima Space Center		Commons
commons	image		Mock-up of H-2B rocket		Commons
commons	image		HIIB F NAGOYA S M		Commons
commons	image		HIIB F NAGOYA S M		Commons
commons	image		H-2B Model in Komaki Air Base 20140223		Commons
commons	image		Nagoya City Science Museum 20150125-2		Commons
commons	image		H-IIB Rocket in front of Nagoya City Science Museum 20150125		Commons
commons	image		Nagoya City Science Museum 20150125-1		Commons
commons	image		Panther of the week: Senior Airman Matthew Greger		Commons
commons	image		H-IIB No. F8 on the launch pad		Commons