ABOUT H-II
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.
PAYLOAD CAPACITY
10,060 kg
TO LEO
22,182 lbs
3,930 kg
TO GTO
8,666 lbs
⚙ RELATED ENGINES
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