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MITSUBISHI HEAVY INDUSTRIES

N-2

8FLIGHTS
100%SUCCESS
8STREAK
Feb 1981FIRST FLIGHT
NOREUSABLE
HEIGHT35 m
DIAMETER2.44 m
LAUNCH MASS132 kg
LIFTOFF THRUST2,278 kN
STAGES3

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.

2,000 kg
TO LEO
4,410 lbs
730 kg
TO GTO
1,610 lbs
2,278
KILONEWTONS
512,115
POUNDS-FORCE
~3,055
HORSEPOWER
Height35 m (115 ft)
Diameter2.44 m (8 ft)
Launch Mass132 kg (291 lbs)
Stages3