Padside

N-2

Mitsubishi Heavy Industries · Retired

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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

Thrust
2,278 kN
Height
35 m
Diameter
2.44 m
Launch mass
132 t
Stages
3
Launch cost
LEO capacity
2,000 kg
GTO capacity
730 kg
GEO capacity
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
8
Launches with a definitive outcome
Success rate
100%
8 of 8
Current success streak
8
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
Between consecutive booster flights

Counted from padside's own launch record — the same basis as the Stats page.

Launches