🚀Launchpad

N-I

Mitsubishi Heavy Industries

Hersteller
Mitsubishi Heavy Industries
Erstflug
1975-09-09
Länge
34 m
Durchmesser
2.44 m
Nutzlast LEO
1.200 kg
Nutzlast GTO
360 kg
Starts
7
Erfolgreich
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.