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Specification	Delta 2313 McDonnell Douglas × remove	Molniya-M 2BL Russian Space Forces × remove
Flights	3	272
Success rate	66.7%	95.2%
Thrust	1,737 kN	—
Height	35 m	—
Diameter	2.44 m	—
Launch mass	131 t	—
LEO capacity	500 kg	—
GTO capacity	—	—
Launch cost	—	—
Reusable	No	No
Stages	3	—

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