Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:basedOn |
gptkb:K-13_missile
|
| gptkbp:countryOfOrigin |
gptkb:China
|
| gptkbp:diameter |
127 mm
|
| gptkbp:enteredService |
1967
|
| gptkbp:exportedTo |
gptkb:Albania
gptkb:Bangladesh gptkb:Egypt gptkb:Iran gptkb:Iraq gptkb:North_Korea gptkb:Pakistan gptkb:Vietnam |
| gptkbp:guidanceSystem |
infrared homing
|
| https://www.w3.org/2000/01/rdf-schema#label |
PL-2
|
| gptkbp:length |
2.83 m
|
| gptkbp:manufacturer |
gptkb:China_Academy_of_Launch_Vehicle_Technology
|
| gptkbp:range |
1.6–8 km
|
| gptkbp:speed |
Mach 2.5
|
| gptkbp:type |
short-range missile
|
| gptkbp:usedBy |
gptkb:People's_Liberation_Army_Air_Force
|
| gptkbp:usedOn |
gptkb:Chengdu_J-7
gptkb:Shenyang_J-6 gptkb:Shenyang_J-8 gptkb:Nanchang_Q-5 Mikoyan-Gurevich MiG-21 (exported version) |
| gptkbp:warheadType |
11.3 kg
|
| gptkbp:weight |
75.6 kg
|
| gptkbp:bfsParent |
gptkb:AIM-9_Sidewinder_(licensed_production)
|
| gptkbp:bfsLayer |
7
|