H-IIB304 / launch vehicle
sourcingtypical 4/5 · 15 factsmedium-lift launch vehicleJPNretired
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.
key specs
payload to LEO //16,500 kg
payload to GTO //8,000 kg
height //56.6 m
price per launch //$112,500,000
flight record //9 / 9 (100.0% success)
figures describe the 304 configuration where sourced
faq
Who builds H-IIB?
H-IIB is built by Mitsubishi Heavy Industries. (source, as of 2026-07-05)
How many times has H-IIB flown?
H-IIB has flown 9 times. (source, as of 2026-07-05)
When did H-IIB first fly?
H-IIB first flew on 2009-09-10. (source, as of 2026-07-05)
Is H-IIB reusable?
H-IIB is not reusable. (source, as of 2026-07-05)
facts
providerMitsubishi Heavy Industries
countryJPN
classmedium-lift launch vehicle
payload to LEO (kg)16500
reusableno
first flight2009-09-10
flights total9
flights successful9
last flight2020-05-20
next flightunknown
statusretired
price per launch (USD)112500000
payload to GTO (kg)8000
height (m)56.6
diameter (m)5.2
mass (kg)551000
events
sources
[1] ll.thespacedevs.com ↗
provider2026-07-05country2026-07-05payload to LEO (kg)2026-07-05reusable2026-07-05first flight2026-07-05flights total2026-07-05flights successful2026-07-05last flight2026-07-05status2026-07-05price per launch (USD)2026-07-05payload to GTO (kg)2026-07-10height (m)2026-07-10diameter (m)2026-07-10mass (kg)2026-07-10
[2] en.wikipedia.org ↗
classwikipedia2026-07-05