The N-II or N-2 was a derivative of the American Delta rocket, produced under licence in Japan. It replaced the N-I-rocket in Japanese use. It used a Thor-ELT first stage, a Delta-F second stage, nine Castor SRMs, and on most flights either a Star-37E or Burner-2 upper stage, identical to the US Delta 0100 series configurations. Eight were launched between 1981 and 1987, before it was replaced by the H-I, which featured Japanese-produced upper stages. All eight launches were successful.
Specifications
- Thrust
- 2,278 kN
- Height
- 35 m
- Diameter
- 2.44 m
- Launch mass
- 132 t
- Stages
- 3
- Launch cost
- —
- LEO capacity
- 2,000 kg
- GTO capacity
- 730 kg
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
8
Launches with a definitive outcome
Success rate
100%
8 of 8
Current success streak
8
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- N-2 | Momo 1a — Success
- N-2 | Yuri 2B — Success
- N-2 | Himawari 3 — Success
- N-2 | Yuri 2A — Success
- N-2 | Sakura 2B — Success