Space · launch vehicle
N-2
MHI
RETIRED
At a glance
Launches
8
Success rate
100%
8 ok · 0 failed
Payload to LEO
2,000 kg
Payload to GTO
730 kg
Manufacturer
Mitsubishi Heavy IndustriesStatus
RetiredFirst flight
11 Feb 1981Reusable
NoHeight
35 mDiameter
2.44 mLaunch mass
132 tLiftoff thrust
2,278 kNStages
3Launch cost
—Booster landings
—Links
WikipediaAbout
The N-II or N-2 was a derivative of the American Delta rocket, produced under licence in Japan. It replaced the N-I-rocket in Japanese use. It used a Thor-ELT first stage, a Delta-F second stage, nine Castor SRMs, and on most flights either a Star-37E or Burner-2 upper stage, identical to the US Delta 0100 series configurations. Eight were launched between 1981 and 1987, before it was replaced by the H-I, which featured Japanese-produced upper stages. All eight launches were successful.
Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026
