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Retired

N-2

N-2

🏭 Mitsubishi Heavy Industries🌐 Japanese📖 Wikipedia
🚀

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.

📊 Specifications

📏Height
35 m
⭕Diameter
2.44 m
⚖️Launch Mass
132 kg
🛰️LEO Capacity
2,000 kg
🌍GTO Capacity
730 kg
🗓️Maiden Flight
Feb 11, 1981
🚀Total Launches
8
✅Success Rate
100%
♻️Reusable
Expendable
🏭Manufacturer
Mitsubishi Heavy Industries
🌐Country
Japanese
📋Status
Retired

📷 Photo Gallery

🚀

🛰️ Launch History