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Specification	Delta 3910/PAM McDonnell Douglas × remove	Molniya-M 2BL Russian Space Forces × remove
Flights	7	272
Success rate	100%	95.2%
Thrust	3,188 kN	—
Height	35 m	—
Diameter	2.44 m	—
Launch mass	191 t	—
LEO capacity	1,087 kg	—
GTO capacity	—	—
Launch cost	—	—
Reusable	No	No
Stages	4	—

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