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Specification	Thor Delta L McDonnell Douglas × remove	Proton K/DM-2 Khrunichev State Research and Production Space Center × remove
Flights	2	110
Success rate	50%	93.6%
Thrust	1,452 kN	—
Height	35 m	—
Diameter	2.44 m	—
Launch mass	89 t	—
LEO capacity	300 kg	—
GTO capacity	300 kg	—
Launch cost	$16.54M	—
Reusable	No	No
Stages	4	—

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