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Specification	Vikram-I Skyroot Aerospace × remove	Proton K/DM-2 Khrunichev State Research and Production Space Center × remove
Flights	1	110
Success rate	100%	93.6%
Thrust	1,200 kN	—
Height	20 m	—
Diameter	1.7 m	—
Launch mass	—	—
LEO capacity	350 kg	—
GTO capacity	—	—
Launch cost	—	—
Reusable	No	No
Stages	4	—

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