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At a glance
Measured figures
R-13M
Single sourceR-3R
Single sourceConfiguration
| Specification | K-13 (missile) | PL-15 |
|---|---|---|
| Type | Short-range infrared homing air-to-air missile[source] | Beyond-visual-range air-to-air missile[source] |
| Place of origin | Soviet Union[source] | People's Republic of China[source] |
| In service | 1961[source] | 2016–present[source] |
| Used by | See Operators[source] | People's Liberation Army Air Force |
2.830 m (9 ft 3.4 in) (R-13M) 3.48 m (11 ft 5 in) (R-3R)[source]
PL-15E
Single source399.6 cm (13 ft 1.3 in) (PL-15E)[source]
R-13M
Single source631 mm (24.8 in) (R-13M)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
People's Liberation Army Naval Air Force[source]Operator listed in the retained article; inventory date not specified
Pakistan Air Force[source]Operator listed in the retained article; inventory date not specified
| Manufacturer | Vympel[source] | China Airborne Missile Academy (CAMA)[source] |
|---|
| Warhead | 7.4 kg (16 lb)[source] | — |
|---|
| Engine | solid-fuel rocket engine[source] | Dual-pulsed solid-propellant rocket[source] |
|---|
| Guidance system | infrared homing[source] | Active radar homing[source] |
|---|
| Launch platform | MiG-21 , MiG-23 , MiG-19 , MiG-17 Sukhoi Su-17/20/22[source] | J-20 , J-35 , J-10C , J-15T , J-16 , J-11BG , JF-17 Block-3[source] |
|---|
| Guidance | (R-3S) infrared homing ; (R-3R) SARH[source] | — |
|---|
| Launch weight | (R-3S) 75 kg (166 lb); (R-3R) 93 kg (205 lb)[source] | — |
|---|
| Explosive content | 5.3 kg (11.68 lbs) of TGAF-5 (40% TNT, 40% RDX, 20% Aluminium powder)[source] | — |
|---|
| Fuze | type 428 proximity fuze and I-107 Contact fuze (R-3R)[source] | — |
|---|
| Former operator · Bulgaria | Bulgaria[source] | — |
|---|
| Former operator · Guinea | Guinea[source] | — |
|---|
| Reported operators |
| — |
|---|
150–200 km (93–124 mi) (PL-15) 145 km (90 mi) (PL-15E)[source]