Mitsubishi Heavy Industries

N-I

Retired

Overview

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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.

Manufacturer

Mitsubishi Heavy Industries

Variant

N/A

Alias

N/A

Maiden Flight

September 9, 1975

Technical Specifications

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34 m

Length

2.44 m

Diameter

0 t

Launch Mass

Liftoff Thrust

1200 kg

LEO Capacity

360 kg

GTO Capacity

Launch Record

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7

Total Launches

6

Successful

1

Failed

85.7%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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