Р-5М (8К51) - ракетный комплекс

The developer of the complex was designated OKB-1 NII-88 under the leadership of Sergey Korolev.
R-5 Pobeda ("Victory") was a theatre ballistic missile developed by the Soviet Union during the Cold War. The R-5M version was assigned the NATO reporting name SS-3 Shyster and carried the GRAU index 8K51.

Start of development April 10, 1954
Manufactured plant number 586 (Dnepropetrovsk)
Flight tests in January 1955-February 1956
Adopted an June 21, 1956 (retired in 1967)
Number of steps 1
Fuel liquid cryogenic component
Type launcher ground launcher
Quantity and power of warheads 1x300 kt
Weight of the warhead / throw weight 1350 kg
The maximum range of 1200 km
Inertial control system with radio
Accuracy to 1.5 km of lateral deflection, 1.25 km in range
Length of 20,7 m
Launch mass 28,6 t
Fuel weight 24,7 t (including hydrogen peroxide)
Liquid oxygen oxidizer
Fuel 92% ethyl alcohol
Traction control (asl / vacuum) 432/500 kN
Specific impulse (asl / vacuum) 2158/2433 m / s
Launch preparation time 2 hours

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