H-IIA 204
JPN Wikipedia 
Built & Operated By
Mitsubishi Heavy Industries
Commercial · founded 1884
Family
H-II
variant IIA 204
Maiden Flight
18 DEC 2006
About
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.
Vehicle Specifications
Height
53 m
Diameter
4 m
Launch Mass
445 T
Stages
2
Configuration
Expendable
Launch Record
Total Launches
1
Successful
1
Failed
0
Consecutive
1
Performance
To GTO
6,000 kg