Brigadier General James Monroe Williams

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. Eight were launched between 1981 and 1987, before it was replaced by the H-I, which featured Japanese-produced upper stages. All eight launches were successful.

Launch history

Flight No. Date / time (UTC) Rocket,
Configuration
Launch site Payload Payload mass Orbit Customer Launch
outcome
7(F) 11 February 1981
08:30
Tanegashima ETS-4 (Kiku-3)[1] GTO Success
8(F) 10 August 1981
20:03
Tanegashima GMS-2 (Himawari-2)[2] GTO Success
10(F) 4 February 1983
08:37
Tanegashima CS-2A (Sakura-2A)[3] GTO Success
11(F) 5 August 1983
20:29
Tanegashima CS-2B (Sakura-2B)[3] GTO Success
12(F) 23 January 1984
07:58
Tanegashima BS-2A (Yuri-2A)[4] GTO Success
13(F) 2 August 1984
20:30
Tanegashima GMS-3 (Himawari-3)[2] GTO Success
14(F) 12 February 1986
07:55
Tanegashima BS-2B (Yuri-2B)[4] GTO Success
16(F) 19 February 1987
01:23
Tanegashima MOS-1 (Momo-1)[5] LEO Success

See also

References

  1. ^ "JAXA | Engineering Test Satellite IV "KIKU-3" (ETS-IV)". JAXA | Japan Aerospace Exploration Agency. Retrieved 2020-03-16.
  2. ^ a b "JAXA | Geostationary Meteorological Satellite "Himawari" (GMS)". JAXA | Japan Aerospace Exploration Agency. Retrieved 2020-03-16.
  3. ^ a b "JAXA | Communication Satellite "Sakura" (CS)". JAXA | Japan Aerospace Exploration Agency. Retrieved 2020-03-16.
  4. ^ a b "JAXA | Broadcasting Satellite "Yuri" (BS)". JAXA | Japan Aerospace Exploration Agency. Retrieved 2020-03-16.
  5. ^ "JAXA | Marine Observation Satellite-1 "Momo-1" (MOS-1)". JAXA | Japan Aerospace Exploration Agency. Retrieved 2020-03-16.