LAUNCHER INFO

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.

MANUFACTURER INFO

Mitsubishi Heavy Industries

LAUNCHER SPECIFICATIONS

(diameter)

2.44 m

TO GTO

730 kg

(length)

35 m

TO LEO

2000 kg

(reusable)

false

LAUNCH STATISTICS