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Specification	Delta II 6925 McDonnell Douglas × remove	Voskhod Soviet Space Program × remove
Flights	13	299
Success rate	100%	95.7%
Thrust	3,981 kN	—
Height	38.1 m	—
Diameter	2.44 m	—
Launch mass	218 t	—
LEO capacity	3,981 kg	—
GTO capacity	1,446 kg	—
Launch cost	—	—
Reusable	No	No
Stages	4	—

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