Rocket
H-I
Japan1986 to 1992
H-I is Japan's step between the licensed N rockets and the fully Japanese H-II: a Thor-Delta-based first stage topped by a new Japanese liquid-hydrogen second stage. From 1986 to 1992 it flies nine times without a failure, launching communications, weather and Earth observation satellites.
- Launches
- 9
- Success rate
- 100%
- 0 failures
- Builder
- MHI
- Height
- 42 m
- Diameter
- 2.4 m
- Stages
- 3
- Boosters
- 9 × Castor 2
- Propellants
- Solid, Kerosene / LOX, LH2 / LOX
- Payload to LEO
- 3,200 kg
- Payload to GTO
- 1,100 kg
Launches per year
Show as table
| Year | Launches |
|---|---|
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 2 |
| 1989 | 1 |
| 1990 | 2 |
| 1991 | 1 |
| 1992 | 1 |