NEXT SPACEFLIGHT

H-I

The H–I or H–1 was a Japanese liquid-fuelled carrier rocket, consisting of a license-built version of the Thor-ELT, which was originally constructed for the US Delta 1000 rocket, and all-Japanese upper stages. The H in the name represented the use of liquid hydrogen fuel in the second stage. It replaced the N-II, and was subsequently replaced by the H–2, which used the same upper stages with a Japanese first stage.

Missions: 9
Successes: 9
Partial Failures: 0
Failures: 0
Success Streak: 9
Success Rate: 100%
Wiki

Configurations

H-I (9 SO)
MHI
Status: Retired
Payload to LEO: 3,200 kg
Payload to GTO: 1,100 kg
Stages: 2
Strap-ons: 9
Rocket Height: 42.0 m
Fairing Diameter: 2.44 m
H-I UM-129A (6SO)
MHI
Status: Retired
Payload to LEO: 3,200 kg
Payload to GTO: 1,100 kg
Stages: 3
Strap-ons: 6
Rocket Height: 42.0 m
Fairing Diameter: 2.44 m
H-I UM-129A (9SO)
MHI
Status: Retired
Payload to LEO: 3,200 kg
Payload to GTO: 1,100 kg
Stages: 3
Strap-ons: 9
Rocket Height: 42.0 m
Fairing Diameter: 2.44 m

Launch Sites

LA-Y1, Tanegashima Space Center, Japan
SLC-N, Tanegashima Space Center, Japan

Launches

MHI
H-I (9 SO) | Fuyo (JERS-1)
Tue Feb 11, 1992 01:50 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
H-I UM-129A (9SO) | Yuri-3B
Sun Aug 25, 1991 08:40 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
H-I UM-129A (9SO) | Yuri-3A
Tue Aug 28, 1990 09:05 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
H-I (9 SO) | Orizuru, Fuji 1b & Momo-1b
Wed Feb 07, 1990 01:33 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
H-I UM-129A (6SO) | Himawari 4
Tue Sep 05, 1989 19:11 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
H-I UM-129A (9SO) | Sakura 3B
Fri Sep 16, 1988 09:59 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
H-I UM-129A (9SO) | Sakura 3A
Fri Feb 19, 1988 10:05 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
H-I UM-129A (9SO) | Kiku 5
Thu Aug 27, 1987 09:20 UTC
LA-Y1, Tanegashima Space Center, Japan
MHI
H-I (9 SO) | Fuji 1a, Jindai & Ajisai
Tue Aug 12, 1986 20:45 UTC
LA-Y1, Tanegashima Space Center, Japan