N-2
MHI
Details
Height
35 m
Diameter
2.44 m
GTO
730 kg
LEO
2,000 kg
Thrust at Liftoff
2,278 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
February 11, 1981
Description
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.