Mitsubishi Heavy Industries

H-IIB 304

304

H-IIB 304
Retired

Overview

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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.

Manufacturer

Mitsubishi Heavy Industries

Variant

304

Alias

N/A

Maiden Flight

September 10, 2009

Technical Specifications

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56.6 m

Length

5.2 m

Diameter

1 t

Launch Mass

9000 kN

Liftoff Thrust

16500 kg

LEO Capacity

8000 kg

GTO Capacity

Launch Record

/03
9

Total Launches

9

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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