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R-13 (missile)

The R-13 was a submarine-launched ballistic missile (SLBM) developed by the Soviet Union starting around 1955. It was assigned the NATO reporting name SS-N-4 Sark and carried the GRAU index 4K50.

History
Development of the R-13 was authorised by the Soviet Supreme Council on 25 July 1955 for use on the Project 629 and Project 658 submarines. The design work was started by OKB-1 under Sergei Korolev before being transferred to CB Miasskoe engineering / Makeyev Rocket Design Bureau (chief designer - Viktor Makeyev). Final technical specifications was approved by 11 January 1956. Serial production was undertaken at Zlatoust Machine-Building Plant in 1959. The R-13 was a single-stage liquid-fuel rocket and entered service in 1961. This missile was somewhat similar in design to the R-11FM missile, which caused some confusion in Western intelligence services during the Cold War. The missiles were phased out from 1965 to 1975. A set of four stabilizers and verniers were used to keep the missile on-course during initial flight. During initial testing before the missiles were deployed, 26 of 32 missiles (81%) were successfully launched. While the systems were deployed from 1961 to 1975, 225 of 311 launches (72%) were successful. ==Operators==
Operators
; • Soviet Navy ==Specifications==
Specifications
• Length: • Diameter: • Diameter (to stabilizers): • Launch weight: 13.7 t • Warhead: single thermonuclear: 1.2 to 2.0 Mt (perhaps as low as 1.0 Mt) • Propulsion: liquid-fuel rocket, single stage • Engine: Isaev S2.713 liquid rocket engine, 252 kN of thrust • Oxidizer: AK-27I • Fuel: TG-02 • Range: about • Launching technique: surfaced • CEP: == See also ==
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