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Space · launch vehicle

H-IIB 304

MHI RETIRED
At a glance
Launches
9
Success rate
100%
9 ok · 0 failed
Payload to LEO
16,500 kg
Payload to GTO
8,000 kg
Status
Retired
First flight
10 Sept 2009
Reusable
No
Height
56.6 m
Diameter
5.2 m
Launch mass
551 t
Liftoff thrust
9,000 kN
Stages
2
Launch cost
$112,500,000
Booster landings
—
About

H-IIB (H2B) is an expendable launch system used to launch H-II Transfer Vehicles (HTV, or Kounotori) towards the International Space Station. H-IIB rockets are liquid-fuelled with solid-fuel strap-on boosters and are launched from the Tanegashima Space Center in Japan. Mitsubishi and JAXA have been primarily responsible for design, manufacture, and operation of H-IIB.