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N-II (rocket)

Spacecraft and Launch Vehicles

The N-II, also written N-2, was a Japanese derivative of the American Delta rocket, produced under licence in Japan, which replaced the N-I in Japanese service. It used a Thor-ELT first stage, a Delta-F second stage and nine Castor solid rocket motors, with a Star-37E or Burner-2 upper stage on most flights, identical to the American Delta 0100 series configurations. Eight were launched between 1981 and 1987 and all eight launches were successful. It was replaced by the H-I, which kept the licence-built first stage but introduced Japanese-produced upper stages, so the N-II was the last of the Japanese rockets whose upper stages were American designs.

Facts
Year
1981 1
Engine Class
Rocket 1
Status
Out of production 1
Connections

Exemplifies

Space Transport, Modes
Source N-II (rocket) (Wikipedia)

Of Make

Source Mitsubishi Heavy Industries (Wikipedia)
Sources
1. N-II (rocket) (Wikipedia)
  • Lead, launches
    Eight were launched between 1981 and 1987
  • Lead, successor
    before it was replaced by the H-I
  • Lead, solid boosters
    nine Castor SRMs
  • Lead
    produced under licence in Japan
View the Source
Mitsubishi Heavy Industries (Wikipedia)
Of Make: Mitsubishi, Products, Space launch vehicles, make
Quote, Of Make: Mitsubishi, Products, Space launch vehicles, make
N-II (with license from McDonnell-Douglas)
View the Source
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