Description
An early Russian rocket designed by Sergei Korolev in the Soviet Union
Specifications
-
Stages
1
-
Length
30.0 m
-
Diameter
2.99 m
-
Fairing Diameter
2.99 m
-
Launch Mass
277.0 T
-
Thrust
3999.0 kN
Family
-
Name
Sputnik 11A59
-
Family
―
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Variant
11A59
-
Alias
―
-
Full Name
Sputnik 11A59
Payload Capacity
-
Launch Cost
―
-
Low Earth Orbit
1400.0 kg
-
Geostationary Transfer
Orbit
―
-
Direct Geostationary
―
-
Sun-Synchronous Capacity
―