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Specification	H-IIA 202 Mitsubishi Heavy Industries × remove	Proton K/DM-2 Khrunichev State Research and Production Space Center × remove
Flights	35	110
Success rate	100%	93.6%
Thrust	2,260 kN	—
Height	53 m	—
Diameter	4 m	—
Launch mass	285 t	—
LEO capacity	10,000 kg	—
GTO capacity	4,100 kg	—
Launch cost	$90M	—
Reusable	No	No
Stages	2	—

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