Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:deployment |
gptkb:Soviet_Strategic_Rocket_Forces
|
| gptkbp:diameter |
1.65 m
|
| gptkbp:engineType |
single-stage
|
| gptkbp:enteredService |
1959
|
| gptkbp:exportedTo |
gptkb:Warsaw_Pact_countries
|
| gptkbp:guidanceSystem |
inertial
|
| gptkbp:launchWeight |
41,000 kg
|
| gptkbp:length |
22.1 m
|
| gptkbp:manufacturer |
gptkb:Yuzhnoye_Design_Bureau
|
| gptkbp:NATOReportingName |
gptkb:SS-4_Sandal
|
| gptkbp:numberBuilt |
over 2,300
|
| gptkbp:platform |
fixed launch site
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:range |
2,080 km
|
| gptkbp:retired |
1993
|
| gptkbp:successor |
gptkb:RSD-10_Pioneer
|
| gptkbp:type |
medium-range ballistic missile
|
| gptkbp:usedIn |
gptkb:Cuban_Missile_Crisis
|
| gptkbp:warheadType |
nuclear
|
| gptkbp:warheadYield |
1 megaton
|
| gptkbp:bfsParent |
gptkb:Operation_Anadyr
|
| gptkbp:bfsLayer |
5
|
| https://www.w3.org/2000/01/rdf-schema#label |
R-12 Dvina missile
|