N-I
Mitsubishi Heavy Industries
Manufacturer
Mitsubishi Heavy Industries
Maiden flight
1975-09-09
Length
34 m
Diameter
2.44 m
Payload to LEO
1,200 kg
Payload to GTO
360 kg
Launches
7
Successful
6
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.
🚀
N-ISuccess
Kiku-4 · National Space Development Agency of Japan
Friday, Sep 3, 1982, 05:00 UTC
🚀
N-ISuccess
Ayame 2 · National Space Development Agency of Japan
Friday, Feb 22, 1980, 08:35 UTC
🚀
N-IFailure
Ayame · National Space Development Agency of Japan
Tuesday, Feb 6, 1979, 08:46 UTC
🚀
N-ISuccess
Ume 2 · National Space Development Agency of Japan
Thursday, Feb 16, 1978, 04:00 UTC
🚀
N-ISuccess
Kiku 2 · National Space Development Agency of Japan
Wednesday, Feb 23, 1977, 08:50 UTC
🚀
N-ISuccess
Ume 1 · National Space Development Agency of Japan
Sunday, Feb 29, 1976, 03:30 UTC
🚀
N-ISuccess
Kiku-1 · National Space Development Agency of Japan
Tuesday, Sep 9, 1975, 05:30 UTC
No media yet. Livestreams usually appear shortly before launch.