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Specification	Delta 3910/PAM McDonnell Douglas × remove	Soyuz U Russian Federal Space Agency (ROSCOSMOS) × remove
Flights	7	714
Success rate	100%	97.2%
Thrust	3,188 kN	—
Height	35 m	51.1 m
Diameter	2.44 m	2.95 m
Launch mass	191 t	313 t
LEO capacity	1,087 kg	6,900 kg
GTO capacity	—	—
Launch cost	—	—
Reusable	No	No
Stages	4	3

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