Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:controls |
rolleron
|
| gptkbp:diameter |
127 mm
|
| gptkbp:enteredService |
1970s
|
| gptkbp:fuzing |
active infrared proximity
|
| gptkbp:guidanceSystem |
infrared homing
|
| https://www.w3.org/2000/01/rdf-schema#label |
AIM-9J
|
| gptkbp:improves |
better maneuverability
improved guidance electronics |
| gptkbp:length |
2.87 m
|
| gptkbp:manufacturer |
gptkb:Raytheon
|
| gptkbp:notableRelease |
gptkb:AIM-9E
|
| gptkbp:partOf |
gptkb:AIM-9_Sidewinder_family
|
| gptkbp:propulsion |
solid fuel rocket
|
| gptkbp:range |
18 km
|
| gptkbp:replacedBy |
gptkb:AIM-9L
|
| gptkbp:speed |
Mach 2.5
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
gptkb:United_States_Navy |
| gptkbp:usedInConflict |
gptkb:Vietnam_War
|
| gptkbp:warheadType |
high-explosive
|
| gptkbp:weight |
85.3 kg
|
| gptkbp:bfsParent |
gptkb:AIM-9_Sidewinder_missile
gptkb:AIM-9_Sidewinder_(licensed_production) gptkb:AIM-9L |
| gptkbp:bfsLayer |
7
|