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Specification	H-II Mitsubishi Heavy Industries × remove	Proton K/DM-2 Khrunichev State Research and Production Space Center × remove
Flights	7	110
Success rate	85.7%	93.6%
Thrust	—	—
Height	49 m	—
Diameter	4 m	—
Launch mass	260 t	—
LEO capacity	10,060 kg	—
GTO capacity	3,930 kg	—
Launch cost	—	—
Reusable	No	No
Stages	2	—

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