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Specification	Delta II 6925-8 McDonnell Douglas × remove	Molniya-M 2BL Russian Space Forces × remove
Flights	1	272
Success rate	100%	95.2%
Thrust	—	—
Height	39 m	—
Diameter	2.44 m	—
Launch mass	219 t	—
LEO capacity	1,500 kg	—
GTO capacity	—	—
Launch cost	—	—
Reusable	No	No
Stages	4	—

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