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SS-9 Scarp

R-36
Dnepr rocket lift-off 1.jpg
Type Intercontinental ballistic missile
Place of origin USSR
Service history
In service 1974–present (only R-36M2 Voevoda variant)
Used by Soviet and Russian Strategic Rocket Forces
Production history
Manufacturer Yuzhny Machine-Building Plant
Specifications
Weight 209,600 kg (462,100 lb)
Length 32.2 m (106 ft)
Diameter 3.05 m (10.0 ft)
Warhead Depending on variant (see variants); the current one (R-36M2 Mod. 5), 10 x 550-750 kiloton MIRV warheads with a large amount of decoys and other penetration aids. Originally (Mod. 1), 1 x 18-25 megaton warhead.
Detonation
mechanism
Airburst

Engine Two-stage liquid propellant
Operational
range
10,200–16,000 km
Speed Mach 23+
Guidance
system
Inertial, autonomous
Accuracy 220–700 m CEP
Launch
platform
Silo

The R-36 (Russian: Р-36) is a family of intercontinental ballistic missiles (ICBMs) and space launch vehicles 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 MIRV (multiple independently targetable reentry vehicle) missile. The later version, the R-36M 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 U.S. 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. Russia intends to replace the R-36 with a new heavy ICBM, the RS-28 Sarmat.

The R-36 (SS-9) is a two-stage rocket powered by a liquid bipropellant, with UDMH as fuel and nitrogen tetroxide as an oxidizer. It carries one of two types of re-entry vehicles (RVs) developed especially for this missile:


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