Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:category |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designer |
gptkb:Sergei_Korolev
|
| gptkbp:diameter |
0.88 m
|
| gptkbp:engineType |
piston engine
|
| gptkbp:enteredService |
1955
|
| gptkbp:guidanceSystem |
inertial
|
| https://www.w3.org/2000/01/rdf-schema#label |
R-11 missile
|
| gptkbp:launchWeight |
5,400 kg
|
| gptkbp:length |
10.3 m
|
| gptkbp:manufacturer |
gptkb:Votkinsk_Machine_Building_Plant
|
| gptkbp:NATOReportingName |
gptkb:SS-1b_Scud-A
|
| gptkbp:platform |
mobile transporter erector launcher
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:range |
270 km
|
| gptkbp:successor |
gptkb:R-17_Elbrus
|
| gptkbp:usedBy |
gptkb:Warsaw_Pact
gptkb:Soviet_Army |
| gptkbp:warheadType |
nuclear
conventional |
| gptkbp:bfsParent |
gptkb:Tactical_Missiles_Corporation
|
| gptkbp:bfsLayer |
5
|