DBSE
Hardware/Vehicles/H-II

H-II

Retired

Mitsubishi Heavy Industries · 2-stage orbital rocket · Part of the H2 family

Total Launches
7
Success Rate
85.7%
Payload to LEO
10.1 t
First Flight
1994
Reusable
No

Specifications

Height49 m
Diameter4 m
Wet Mass260,000 kg
Payload to GTO3.9 t
Payload to SSON/A
ManufacturerMitsubishi Heavy Industries
CountryJapan

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

Reliability by Year

Related Entities

H-IIA 202Vehicle familyH-IIA 204Vehicle familyMitsubishi Heavy IndustriesManufacturerSRB-AEngine

Data Sources for This Record

Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata