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, 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