H-II

The H-II (H2) rocket was a Japanese satellite launch system, which flew seven times between 1994 and 1999, with five successes. It was developed by NASDA in order to give Japan a capability to launch larger satellites in the 1990s. It was the first two-stage liquid-fuelled rocket Japan made using only technologies developed domestically. It was superseded by the H-IIA rocket following reliability and cost issues.

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Wikimedia, Wikidata
H-2; H2
medium-lift launch vehicle, expendable launch vehicle, liquid-propellant rocket, two-stage-to-orbit, Mitsubishi Heavy Industries, 
Sikh Confederacy, Republic of Haiti, medium-lift launch vehicle, B, A, expendable launch vehicle, Ekran, Dong Fang Hong 2, Tarshish, Sweden, Ashkenaz, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Japan, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, 

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Location: KML, Cluster Map, Maps,

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  H-IIA ⓘ
  Japanese expendable medium-lift launch vehicle

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  H-IIB ⓘ
  Japanese expendable launch system used to launch H-II Transfer Vehicles

Frameless

Tanegashima Space Center

OREX mockup in H-II rocket fairing 02 (cropped)

H-II F7 01

H-II F7 02

LE-7 rocket engine

H-II rocket kakuda

H-II rocket at the TKSC

ロケット - panoramio

角田市の台山公園 - panoramio

スペースタワーコスモハウス - panoramio

Type	Subtype	Date	Description	Notes	Source
class	rocket		H-IIA	H-II	Wikidata
class	rocket		H-IIB	H-II	Wikidata
commons	image		Tanegashima Space Center		Commons
commons	image		OREX mockup in H-II rocket fairing 02 (cropped)		Commons
commons	image		H-II F7 01		Commons
commons	image		H-II F7 02		Commons
commons	image		LE-7 rocket engine		Commons
commons	image		H-II rocket kakuda		Commons
commons	image		H-II rocket at the TKSC		Commons
commons	image		ロケット - panoramio		Commons
commons	image		角田市の台山公園 - panoramio		Commons
commons	image		スペースタワーコスモハウス - panoramio		Commons