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Specification	Start Moscow Institute of Thermal Technology × remove	Proton K/DM-2 Khrunichev State Research and Production Space Center × remove
Flights	1	110
Success rate	0%	93.6%
Thrust	887 kN	—
Height	28.9 m	—
Diameter	1.61 m	—
Launch mass	60 t	—
LEO capacity	645 kg	—
GTO capacity	—	—
Launch cost	$10.5M	—
Reusable	No	No
Stages	5	—

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