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H-I

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Launch history

Flight № Date / time (UTC) Rocket,
Configuration
Launch site Payload Payload mass Orbit Customer Launch
outcome
15(F) 12 August 1986,
20:45
H-I Osaki Launch Complex EGP (Ajisai) LEO Success
9 SRMs, 2 stages
17(F) 27 August 1987,
09:20
H-I Osaki Launch Complex ETS-5 (Kiku-5) GTO Success
9 SRMs, 3 stages
18(F) 19 February 1988,
10:05
H-I Osaki Launch Complex CS-3A (Sakura-3A) GTO Success
9 SRMs, 3 stages
19(F) 16 September 1988,
09:59
H-I Osaki Launch Complex CS-3B (Sakura-3B) GTO Success
9 SRMs, 3 stages
20(F) 5 September 1989,
19:11
H-I Osaki Launch Complex GMS-4 (Himawari-4) GTO Success
6 SRMs, 3 stages
21(F) 7 February 1990,
01:33
H-I Osaki Launch Complex MOS-1B (Momo-1B) LEO Success
9 SRMs, 2 stages
22(F) 28 August 1990,
09:05
H-I Osaki Launch Complex BS-3A (Yuri-3A) GTO Success
9 SRMs, 3 stages
23(F) 25 August 1991,
08:40
H-I Osaki Launch Complex BS-3B (Yuri-3B) GTO Success
9 SRMs, 3 stages
24(F) 11 February 1992,
01:50
H-I Osaki Launch Complex JERS-1 (FUYO-1) LEO Success
9 SRMs, 2 stages

When the H–1 was announced in 1986, company representative Tsuguo Tatakawe clarified that it would only be used to launch indigenous (i.e. Japanese) payloads, that only two launches per year could be mounted, and that the launch window consisted of a four-month period in which Japanese fishing fleets were not active (the falling launch boosters may damage fishing nets in the ocean waters).[1]

See also

References

  1. ^ Japan's H–1 and H–2 rockets, Air & Space/Smithsonian, February/March 1987, p. 19
  • Wade, Mark. "Delta". Encyclopedia Astronautica. Archived from the original on 22 May 2013. Retrieved 31 August 2008. {{cite web}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)
  • McDowell, Jonathan. "Thor". Orbital and Suborbital Launch Database. Jonathan's Space Report. Retrieved 31 August 2008.
  • Krebs, Gunter. "H-1". Gunter's Space Page. Retrieved 31 August 2008.