Mitsubishi Heavy Industries

N-2

2

Retired

Overview

/01

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.

Manufacturer

Mitsubishi Heavy Industries

Variant

2

Alias

N/A

Maiden Flight

February 11, 1981

Technical Specifications

/02
35 m

Length

2.44 m

Diameter

0 t

Launch Mass

2278 kN

Liftoff Thrust

2000 kg

LEO Capacity

730 kg

GTO Capacity

Launch Record

/03
8

Total Launches

8

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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