N-I
MHI
Details
Height
34 m
Diameter
2.44 m
GTO
360 kg
LEO
1,200 kg
Thrust at Liftoff
Unknown
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
September 9, 1975
Description
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.