Launcher

H-IIB

Expendable two-stage hydrolox medium-lift launcher in the H-II launcher family of Japanese launchers, used to launch to the H-II Transfer Vehicle (HTV).

Launcher Info

Status
No Longer in Use
Maximum Performance
Medium-Lift
Type
Rocket Launcher
Reusability

Launcher Cofigurations

Related Links

No items found.

Additional Background

Though it had larger diameter than the H-IIA launcher, the H-IIB launcher was derived from the H-IIA. JAXA and MHI Launch Services sought to take the learning from developing the H-IIA and apply it to a launcher which could handle the needs of cargo re-supply to the International Space Station. After the HTV was retired, the H-IIB launcher was as well, given that it no longer had a purpose.

Launches From

Engines

Common Payloads

Company

Operated By

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Service History

The H-IIB saw nine lauches between 2009 and 2020, all successful. The payload in all cases was the HTV on a mission for providing cargo re-supply to the International Space Station. These missions were operated by JAXA.

Development History

Derived from learning coming from the development and operation of the H-IIA, the H-IIB was designed specifically to support launch of the HTV spacecraft for re-supply of the International Space Station.

Launch Manifest

No items found.

Launch History

No items found.
H-IIB Standard
Only configuration for the H-IIB launcher.
Configuration Service Status
No Longer in Service
Mass to LEO Classification
Medium-Lift
Performance
Orbit
Mass to Orbit (kg)
Low-Earth Orbit (LEO)
19000
No Data
Sun-Synchronous Orbit (SSO)
8000
No Data
Geostationary Transfer Orbit (GTO)
No Data
Geostationary Orbit (GSO)
No Data
Lunar Transfer Orbit (LTO)
No Data
Mars Transfer Orbit (MTO)
No Data
Specs
Orbit
Mass to Orbit (kg)
Length
56.6
No Data
Diameter
56.6
No Data
Dry Mass
No Data
Pressurized Volume
No Data
No detailed launcher stage information is available.