Mitsubishi Heavy Industries
N-2
2
Retired
Overview
/01The 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
Mitsubishi Heavy Industries
Variant
2
Alias
N/A
Maiden Flight
February 11, 1981
Technical Specifications
/0235 m
Length
2.44 m
Diameter
0 t
Launch Mass
2278 kN
Liftoff Thrust
2000 kg
LEO Capacity
730 kg
GTO Capacity
Launch Record
/038
Total Launches
8
Successful
0
Failed
100.0%
Success Rate
0
Attempted Landings
0
Successful Landings
0
Failed Landings
0
Consecutive Successes