Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:compatibleWith |
gptkb:aircraft
gptkb:F-5_Tiger_II F-4 Phantom II |
| gptkbp:diameter |
127 mm
|
| gptkbp:enteredService |
late 1970s
|
| gptkbp:feature |
improved all-aspect capability
improved guidance and counter-countermeasures |
| gptkbp:guidanceSystem |
infrared homing
|
| gptkbp:length |
2.87 m
|
| gptkbp:manufacturer |
gptkb:Raytheon
|
| gptkbp:notableRelease |
gptkb:AIM-9P
|
| gptkbp:origin |
gptkb:United_States
|
| gptkbp:partOf |
gptkb:AIM-9_Sidewinder_family
|
| gptkbp:propulsion |
solid fuel rocket
|
| gptkbp:range |
up to 18 km
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
various NATO countries |
| gptkbp:warheadType |
high-explosive
|
| gptkbp:weight |
85.3 kg
|
| gptkbp:bfsParent |
gptkb:AIM-9_Sidewinder_(licensed_production)
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
AIM-9P-3
|