R-36 (missile)
Type of intercontinental ballistic missile designed by the Soviet Union / From Wikipedia, the free encyclopedia
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The R-36 (Russian: Р-36) is a family of intercontinental ballistic missiles (ICBMs) and space launch vehicles (Tsyklon) designed by the Soviet Union during the Cold War. The original R-36 was deployed under the GRAU index 8K67 and was given the NATO reporting name SS-9 Scarp. It was able to carry three warheads and was the first Soviet MRV (multiple re-entry vehicle) missile.[4] The later version, the R-36M, also known as RS20, was produced under the GRAU designations 15A14 and 15A18 and was given the NATO reporting name SS-18 Satan. This missile was viewed by certain United States analysts as giving the Soviet Union first strike advantage over the U.S., particularly because of its rapid silo-reload ability, very heavy throw weight and extremely large number of re-entry vehicles. Some versions of the R-36M were deployed with 10 warheads and up to 40 penetration aids and the missile's high throw-weight made it theoretically capable of carrying more warheads or penetration aids. Contemporary U.S. missiles, such as the Minuteman III, carried up to three warheads at most.
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R-36 | |
---|---|
Type | Intercontinental ballistic missile |
Place of origin | Soviet Union |
Service history | |
In service | 1966–1979 (original variant) 1988–present (R-36M2 Voevoda variant) |
Used by | Russian Strategic Rocket Forces |
Production history | |
Designed | From 1962 |
Manufacturer | Factory: Yuzhny Machine-Building Plant Developer: Yuzhnoye Design Office |
Unit cost | $7,000,000 |
Specifications | |
Mass | 209,600 kg (462,100 lb) |
Length |
|
Diameter | 3,050 mm (120 in) |
Warhead | Depending on variant (see variants). Newest (R-36M2), 10 × 550–750 kiloton MIRV warheads with a large amount of decoys and other penetration aids. Originally (R-36), 1 × 8–20 megaton warhead. |
Engine | Two or often three liquid fueled rocket stages First Stage: Second Stage: Third Stage: |
Propellant | N2O4/UDMH |
Operational range | 10,200–16,000 km |
Guidance system | Inertial, autonomous |
Accuracy | 220–1,300 m CEP |
Launch platform | Silo |
The R-36 became the base for the Tsyklon launch vehicles family. As of early 2021, Cyclone-4M, the last Tsyklon variant in development, is planned for launch in 2023 from Canso, Nova Scotia.[5]
Some R-36 missiles have been converted into Dnepr medium-lift launch vehicles, capable of putting up to 4,500 kg into orbit.