Vehicle / SINCE 1981

N-2

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.

SPECIFICATIONS 10
Length 35 m
Diameter 2.44 m
Launch Mass T 132
Leo Capacity 2,000 kg
Gto Capacity 730 kg
Thrust 2,278 kN
Reusable No
Total Launches 8
Successful Launches 8
Maiden Flight 1981-02-11