NEXT SPACEFLIGHT

N-II

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.

Missions: 8
Successes: 8
Partial Failures: 0
Failures: 0
Success Streak: 8
Success Rate: 100%
Wiki

Configurations

N-II
MHI
Status: Retired
Payload to LEO: 2,000 kg
Payload to GTO: 730 kg
Stages: 2
Strap-ons: 9
Rocket Height: 35.0 m
N-II Star-37E
MHI
Status: Retired
Payload to LEO: 2,000 kg
Payload to GTO: 730 kg
Stages: 3
Strap-ons: 9
Rocket Height: 35.0 m

Launch Sites

LA-Y1, Tanegashima Space Center, Japan

Launches

MHI
N-II | Momo 1a
Thu Feb 19, 1987 01:23 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
N-II Star-37E | Yuri 2b
Wed Feb 12, 1986 07:55 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
N-II Star-37E | Himawari 3
Thu Aug 02, 1984 20:30 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
N-II Star-37E | Yuri 2a
Mon Jan 23, 1984 07:58 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
N-II Star-37E | Sakura 2b
Fri Aug 05, 1983 20:29 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
N-II Star-37E | Sakura 2a
Fri Feb 04, 1983 08:37 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
N-II Star-37E | Himawari 2
Mon Aug 10, 1981 20:03 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
N-II Star-37E | Kiku 3
Wed Feb 11, 1981 08:30 UTC
LA-Y1, Tanegashima Space Center, Japan