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Specification	Thor Delta A McDonnell Douglas × remove	Molniya-M 2BL Russian Space Forces × remove
Flights	2	272
Success rate	100%	95.2%
Thrust	667 kN	—
Height	31 m	—
Diameter	2.44 m	—
Launch mass	50 t	—
LEO capacity	250 kg	—
GTO capacity	68 kg	—
Launch cost	$9.59M	—
Reusable	No	No
Stages	3	—

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