Orbital launch vehicle

H-1

The H-1 was a Japanese liquid-fuelled carrier rocket, consisting of a license-produced American First Stage and set of booster rockets and all-Japanese upper stages. It replaced the N-II and was subsequently replaced by the H-2 which has the same upper stages with a Japaense first stage.

Flights flown9
Success rate100%9/9
Payload to LEO3,200kg
Maiden flight1986-08-12
Peak year19882 flights

H-1 is built by Mitsubishi Heavy Industries of Japan. Company background, funding, contracts and news for this operator are tracked on Space Index. It first flew on 12 August 1986 and last flew on 11 February 1992.

Flight record

9 records
100% success rate9 of 9 flown
1986peak 1988 · 2 flights1992
First flight1986-08-12
Latest flight1992-02-11
Failures0
Consecutive successes9
Fastest turnaround154d 6h

Payload

Per mission profile
Low Earth orbit3,200kg
Geostationary transfer orbit1,100kg

Vehicle

I spec
Stages3
Length42m
Diameter2.44m
Launch mass142t
Maiden flight1986-08-12
ReusableNo

Pads used

1 pad

Orbits delivered

3 orbits
Geostationary Orbit6Low Earth Orbit2Sun-Synchronous Orbit1

Launch history

9 launches
DateMissionPadOrbitOutcome
1992-02-11H-1 | Fuyo 1Osaki Launch ComplexSun-Synchronous OrbitSuccess
1991-08-25H-1 | Yuri 3BOsaki Launch ComplexGeostationary OrbitSuccess
1990-08-28H-1 | Yuri 3AOsaki Launch ComplexGeostationary OrbitSuccess
1990-02-07H-1 | Momo 1bOsaki Launch ComplexLow Earth OrbitSuccess
1989-09-05H-1 | Himawari 4Osaki Launch ComplexGeostationary OrbitSuccess
1988-09-16H-1 | Sakura 3BOsaki Launch ComplexGeostationary OrbitSuccess
1988-02-19H-1 | Sakura 3AOsaki Launch ComplexGeostationary OrbitSuccess
1987-08-27H-1 | Kiku 5Osaki Launch ComplexGeostationary OrbitSuccess
1986-08-12H-1 | AjisaiOsaki Launch ComplexLow Earth OrbitSuccess

Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.

Further reading: Wikipedia