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This page records N-I | Ume 1 and its reported outcome: Launch Successful. The date above is a historical record.
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Status reported by the mission data provider.
Japanese ionospheric research satellite
Published configuration and flight history.
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.
This is a mission record, not an upcoming calendar appointment.
A single scheduled moment. The schedule may change before launch.
Tanegashima Space Center, Japan
Explore the launch pad, then pull back to see the shape of the destination orbit.
Understand this orbit
Links supplied by the mission data provider.
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