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Launch Vehicle

N-2

retired
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Specifications

Status
retired
Height
35 m
Diameter
2.44 m
Mass
132,000 kg
Stages
3
Payload to LEO
2,000 kg
Payload to GTO
730 kg
First flight
1981-02-11
Total launches
8
Success / Fail
8 / 0

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.

Payloads it launched · 8

MOMO-1 (MOS-1)
LEO
YURI-2B (BS-2B)
GEO
HIMAWARI-3 (GMS-3)
GEO
YURI-2A (BS-2A)
GEO
SAKURA-2B (CS-2B)
GEO
SAKURA-2A (CS-2A)
GEO
HIMAWARI-2 (GMS-2)
GEO
KIKU-3 (ETS-IV)
MEO