H-IIA 204 Vehicle Overview
A complete overview of the H-IIA 204 launch vehicle, including launch stats, vehicle info and launch locations.
Basic Info
Name
H-IIA 204
Family
H-II
Manufacturer
First Launch
18 Dec 2006
Successful Launches
1
Failed Launches
0
Rocket Info
Status
Active
Stages
2
Length
53 m
Diameter
4 m
Launch Mass
445 tons
Reusability
Not Reusable
Payload Info
GTO Capacity
6,000 kg
The H-IIA rocket family is an expendable launch system operated by Mitsubishi Heavy Industries for the Japan Aerospace Exploration Agency. The liquid fuelled rocket has been used to launch satellites, lunar spacecraft and planetary science craft.