Mitsubishi Heavy Industries
N-I
Retired
Overview
/01The 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.
Manufacturer
Mitsubishi Heavy Industries
Variant
N/A
Alias
N/A
Maiden Flight
September 9, 1975
Technical Specifications
/0234 m
Length
2.44 m
Diameter
0 t
Launch Mass
—
Liftoff Thrust
1200 kg
LEO Capacity
360 kg
GTO Capacity
Launch Record
/037
Total Launches
6
Successful
1
Failed
85.7%
Success Rate
0
Attempted Landings
0
Successful Landings
0
Failed Landings
0
Consecutive Successes