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Space · launch vehicle

N-2

MHI RETIRED
At a glance
Launches
8
Success rate
100%
8 ok · 0 failed
Payload to LEO
2,000 kg
Payload to GTO
730 kg
Status
Retired
First flight
11 Feb 1981
Reusable
No
Height
35 m
Diameter
2.44 m
Launch mass
132 t
Liftoff thrust
2,278 kN
Stages
3
Launch cost
—
Booster landings
—
About

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.