Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:diameter |
127 mm
|
| gptkbp:engine |
gptkb:Hercules/Bermite_Mk_36_solid-fuel_rocket_motor
|
| gptkbp:enteredService |
1982
|
| gptkbp:exportedTo |
multiple allied nations
|
| gptkbp:guidanceSystem |
infrared homing
|
| https://www.w3.org/2000/01/rdf-schema#label |
AIM-9M
|
| gptkbp:improves |
improved counter-countermeasures
improved guidance and control section reduced smoke motor |
| gptkbp:length |
2.87 m
|
| gptkbp:manufacturer |
gptkb:Raytheon
|
| gptkbp:notableRelease |
gptkb:AIM-9L
|
| gptkbp:partOf |
gptkb:AIM-9_Sidewinder_family
|
| gptkbp:range |
18 km
|
| gptkbp:replacedBy |
gptkb:AIM-9X
|
| gptkbp:speed |
Mach 2.5
|
| gptkbp:usedBy |
gptkb:NATO
gptkb:United_States_Air_Force gptkb:United_States_Navy |
| gptkbp:usedInConflict |
gptkb:Gulf_War
gptkb:Operation_Iraqi_Freedom gptkb:Kosovo_War |
| gptkbp:warheadType |
9.4 kg
annular blast fragmentation |
| gptkbp:weight |
85.3 kg
|
| gptkbp:bfsParent |
gptkb:sidewinder
|
| gptkbp:bfsLayer |
6
|