N-2
Mitsubishi Heavy Industries
Manufacturer
Mitsubishi Heavy Industries
Maiden flight
1981-02-11
Length
35 m
Diameter
2.44 m
Payload to LEO
2,000 kg
Payload to GTO
730 kg
Launches
8
Successful
8
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.
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N-2Success
Momo 1a · National Space Development Agency of Japan
Thursday, Feb 19, 1987, 01:23 UTC
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N-2Success
Yuri 2B · National Space Development Agency of Japan
Wednesday, Feb 12, 1986, 07:55 UTC
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N-2Success
Himawari 3 · National Space Development Agency of Japan
Thursday, Aug 2, 1984, 20:30 UTC
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N-2Success
Yuri 2A · National Space Development Agency of Japan
Monday, Jan 23, 1984, 07:58 UTC
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N-2Success
Sakura 2B · National Space Development Agency of Japan
Friday, Aug 5, 1983, 20:29 UTC
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N-2Success
Sakura 2A · National Space Development Agency of Japan
Friday, Feb 4, 1983, 08:37 UTC
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N-2Success
Himawari 2 · National Space Development Agency of Japan
Monday, Aug 10, 1981, 20:03 UTC
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N-2Success
Kiku-3 · National Space Development Agency of Japan
Wednesday, Feb 11, 1981, 08:30 UTC
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