Mitsubishi Heavy Industries
H-IIB 304
304

Retired
Overview
/01H-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.
Manufacturer
Mitsubishi Heavy Industries
Variant
304
Alias
N/A
Maiden Flight
September 10, 2009
Technical Specifications
/0256.6 m
Length
5.2 m
Diameter
1 t
Launch Mass
9000 kN
Liftoff Thrust
16500 kg
LEO Capacity
8000 kg
GTO Capacity
Launch Record
/039
Total Launches
9
Successful
0
Failed
100.0%
Success Rate
0
Attempted Landings
0
Successful Landings
0
Failed Landings
0
Consecutive Successes