H-1
| Status | Retired |
|---|---|
| Country | Japan |
| Manufacturer | Mitsubishi Heavy Industries |
| Number of orbital launches | 9 |
| First launch | 1986-08-12 |
| Last launch | 1992-02-11 |
Launches by year:
Launches:
| Launch date | Launch site | Rocket / Variant | Payload | Notes | Status |
|---|---|---|---|---|---|
| 1992-02-11 | Tanegashima | H-1 | JERS 1 (Fuyo) | success | |
| 1991-08-25 | Tanegashima | H-1 | BS 3b (Yuri 3b) | success | |
| 1990-08-28 | Tanegashima | H-1 | BS 3a (Yuri 3a) | success | |
| 1990-02-07 | Tanegashima | H-1 | MOS 1b (Momo 1b) / DEBUT (Orizuru) / JAS 1b (Fuji 1b, OSCAR 20) | success | |
| 1989-09-05 | Tanegashima | H-1 | GMS 4 (Himawari 4) | success | |
| 1988-09-16 | Tanegashima | H-1 | CS 3A (Sakura 3A) | success | |
| 1988-02-19 | Tanegashima | H-1 | CS 3a (Sakura 3A) | success | |
| 1987-08-27 | Tanegashima | H-1 | ETS 5 (Kiku 5) | success | |
| 1986-08-12 | Tanegashima | H-1 | EGS (Ajisai) / JAS 1a (Fuji 1a, OSCAR 12) / MABES (Jindai) | success | |
Variants:
(This section is under construction)H-1 Base variant
| First launch | 1986-08-12 |
|---|---|
| Mass | 142.26 t |
| Height | 42 m |
Payload capacity:
| LEO | 3200 kg to 185 km |
|---|---|
| GTO | 1100 kg |