
Rocket file · LV-320
H-II
Photograph: Masamic · CC BY-SA 3.0 · licence
H-II is an expendable launch vehicle built by Mitsubishi Heavy Industries. It stands 49.0 m tall, lifts 10,060 kg to low Earth orbit, first flew on 3 February 1994. It has flown 7 times with 6 successes, a success rate of 85.7%. It has nothing on the Launch Library 2 schedule right now.
Specification
Vehicle spec sheet
As listed by Launch Library 2. The cost is Launch Library’s figure, not a quoted price. Figures for rockets outside the sixty most-flown were last read on 2026-11-05.
Flight record
Reliability
About H-II
The H-II rocket was a Japanese satellite launch system which flew seven times between 1994 and 1999 with 5 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 domestic technologies.
Upcoming flights
Manifest
H-II is retired, and no flight is filed.
All upcoming launchesH-II in the archive
From NASA's public image library and Wikimedia Commons. Each photo shows the credit its licence asks for and links back to where it came from.
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Common questions
- How many times has H-II flown?
- 7 times, with 6 successes and 1 failures.
- What is H-II's success rate?
- 85.7%. That's 6 successful flights out of 7 attempts.
- How much can H-II lift to orbit?
- Launch Library 2 lists H-II at 10,060 kg to low Earth orbit and 3,930 kg to geostationary transfer orbit.
- Is H-II reusable?
- No. Launch Library 2 lists H-II as expendable, so no stage is recovered to fly again.
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