🚀Launchpad

N-I

Mitsubishi Heavy Industries

Manufacturer
Mitsubishi Heavy Industries
Maiden flight
1975-09-09
Length
34 m
Diameter
2.44 m
Payload to LEO
1,200 kg
Payload to GTO
360 kg
Launches
7
Successful
6

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.