Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
gptkb:surface-to-air_missile |
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.85 m
|
| gptkbp:elevation |
24 km
|
| gptkbp:enteredService |
1965
|
| gptkbp:guidanceSystem |
radio command
|
| gptkbp:length |
8.8 m
|
| gptkbp:manufacturer |
gptkb:NPO_Novator
|
| gptkbp:NATOReportingName |
gptkb:Ganef
|
| gptkbp:platform |
gptkb:aircraft
|
| gptkbp:propulsion |
gptkb:piston_engine
liquid-fuel sustainer |
| gptkbp:range |
50 km
|
| gptkbp:serviceHistory |
gptkb:Cold_War
|
| gptkbp:Soviet_designation |
gptkb:2K11_Krug
|
| gptkbp:status |
retired
|
| gptkbp:type |
high-altitude
medium-range |
| gptkbp:usedBy |
gptkb:Iraq
gptkb:Syria gptkb:Soviet_Army gptkb:Warsaw_Pact_countries |
| gptkbp:warheadType |
high-explosive fragmentation
|
| gptkbp:weight |
2,450 kg
|
| gptkbp:bfsParent |
gptkb:Ramjet
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
SA-4 Ganef missile
|