N-I
Mitsubishi Heavy Industries
Hersteller
Mitsubishi Heavy Industries
Erstflug
1975-09-09
Länge
34 m
Durchmesser
2.44 m
Nutzlast LEO
1.200 kg
Nutzlast GTO
360 kg
Starts
7
Erfolgreich
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.
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N-ISuccess
Kiku-4 · National Space Development Agency of Japan
Freitag, 03.09.1982, 05:00 UTC
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N-ISuccess
Ayame 2 · National Space Development Agency of Japan
Freitag, 22.02.1980, 08:35 UTC
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N-IFailure
Ayame · National Space Development Agency of Japan
Dienstag, 06.02.1979, 08:46 UTC
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N-ISuccess
Ume 2 · National Space Development Agency of Japan
Donnerstag, 16.02.1978, 04:00 UTC
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N-ISuccess
Kiku 2 · National Space Development Agency of Japan
Mittwoch, 23.02.1977, 08:50 UTC
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N-ISuccess
Ume 1 · National Space Development Agency of Japan
Sonntag, 29.02.1976, 03:30 UTC
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N-ISuccess
Kiku-1 · National Space Development Agency of Japan
Dienstag, 09.09.1975, 05:30 UTC
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