H-II
MHI
Details
Height
49 m
Diameter
4 m
GTO
3,930 kg
LEO
10,060 kg
Thrust at Liftoff
Unknown
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
February 3, 1994
Description
The H-II rocket was a Japanese satellite launch system which flew seven times between 1994 and 1999 with 5 successes. It was developed by NASDA in order to give Japan a capability to launch larger satellites in the 1990s. It was the first two stage liquid fuelled rocket Japan made using only domestic technologies.