H-IIB 304
MHI
Details
Height
56.6 m
Diameter
5.2 m
GTO
8,000 kg
LEO
16,500 kg
Thrust at Liftoff
9,000 kN
Apogee
Unknown
Launch Cost
$112.5M
Maiden Flight
September 10, 2009
Description
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.