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MITSUBISHI HEAVY INDUSTRIES

N-I

7FLIGHTS
85.7%SUCCESS
1FAILURES
2STREAK
Sep 1975FIRST FLIGHT
NOREUSABLE
HEIGHT34 m
DIAMETER2.44 m
LAUNCH MASS131 kg
STAGES3

The N-I or N-1 was a derivative of the American Thor-Delta rocket, produced under licence in Japan. It used a Thor-ELT first stage, a Mitsubishi Heavy Industries-designed LE-3 engine was used as a second stage, and three Castor SRMs. Seven were launched between 1975 and 1982, before it was replaced by the N-II.

1,200 kg
TO LEO
2,646 lbs
360 kg
TO GTO
794 lbs
Height34 m (112 ft)
Diameter2.44 m (8 ft)
Launch Mass131 kg (289 lbs)
Stages3