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R-12 Dvina

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Also known as Dvina, 8K63, SS-4 Sandal, Sandal, SS4

Soviet intercontinental ballistic missile

Key facts

Type
Medium-range ballistic missile
In service
4 March 1959–1993
Manufacturer
Yuzhmash
Unit cost
unknown
Mass
Fully loaded: 41.7 t , Empty: 3.15 t
Length
22,100 mm
Diameter
1,650 mm
Wingspan
2,940 mm (116 in)
Warhead
Thermonuclear
Blast yield
1.0–2.3 Mt
Engine
RD-214 , 635.2 kilonewtons (142,800 lbf)
Payload capacity
1.6 t
Propellant
liquid ( AK-27I / TM-185 )
Fuel capacity
37 t
Operational range
2,000–2,500 km (1,200–1,600 mi)
Maximum speed of vehicle or missile span
3,530 m/s (Mach 10)
Guidance system
autonomous inertial
Accuracy
2.4–5.16 km (1.49–3.21 mi) CEP

via Wikipedia infobox

Wikidata facts

Named after
Daugava
Country of origin
Soviet Union
Manufacturer
Pivdenmash
Image
Soviet-R-12-nuclear-ballistic missile.jpg
Show 4 more facts
Commons category
R-12
NATO reporting name
Sandal
service entry
1959-03-04
total produced
2300
Sources (2)

via Wikidata · CC0

~11 min read

Encyclopedic overview

The cupola of the underground R-12U launching silo in Plokštinė missile base, Lithuania The R-12 Dvina was a theatre ballistic missile developed and deployed by the Soviet Union during the Cold War. Its GRAU designation was 8K63 (8K63U or 8K63У in Cyrillic for silo-launched version), and it was given the NATO reporting name of SS-4 Sandal. The R-12 rocket provided the Soviet Union with the capability to attack targets at medium ranges with a megaton-class thermonuclear warhead and constituted the bulk of the Soviet offensive missile threat to Western Europe. Deployments of the R-12 missile in Cuba caused the Cuban Missile Crisis in 1962. A total of 2335 missiles were produced; all were destroyed in 1993 under the START II treaty.

As well as the single-stage ballistic technology, the R-12 Dvina had a two-stage capability that allowed payloads to be placed into low Earth orbit.

Excerpted from Wikipedia’s “R-12 Dvina” article, available under the CC BY-SA 4.0 licence.