N-2
Mitsubishi Heavy Industries
Hersteller
Mitsubishi Heavy Industries
Erstflug
1981-02-11
Länge
35 m
Durchmesser
2.44 m
Nutzlast LEO
2.000 kg
Nutzlast GTO
730 kg
Starts
8
Erfolgreich
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.
🚀
N-2Success
Momo 1a · National Space Development Agency of Japan
Donnerstag, 19.02.1987, 01:23 UTC
🚀
N-2Success
Yuri 2B · National Space Development Agency of Japan
Mittwoch, 12.02.1986, 07:55 UTC
🚀
N-2Success
Himawari 3 · National Space Development Agency of Japan
Donnerstag, 02.08.1984, 20:30 UTC
🚀
N-2Success
Yuri 2A · National Space Development Agency of Japan
Montag, 23.01.1984, 07:58 UTC
🚀
N-2Success
Sakura 2B · National Space Development Agency of Japan
Freitag, 05.08.1983, 20:29 UTC
🚀
N-2Success
Sakura 2A · National Space Development Agency of Japan
Freitag, 04.02.1983, 08:37 UTC
🚀
N-2Success
Himawari 2 · National Space Development Agency of Japan
Montag, 10.08.1981, 20:03 UTC
🚀
N-2Success
Kiku-3 · National Space Development Agency of Japan
Mittwoch, 11.02.1981, 08:30 UTC
Noch keine Medien vorhanden. Livestreams erscheinen meist kurz vor dem Start.