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At a glance
Measured figures
Length
Single source249 cm (8 ft 2 in)[source]
PL-15E
Single sourceConfiguration
| Specification | AGM-65 Maverick | PL-15 |
|---|---|---|
| Type | Air-to-surface missile[source] | Beyond-visual-range air-to-air missile[source] |
| Place of origin | United States[source] | People's Republic of China[source] |
| In service | 30 August 1972 – present[source] | 2016–present[source] |
| Used by | >30 countries[source] | People's Liberation Army Air Force |
399.6 cm (13 ft 1.3 in) (PL-15E)[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
| Wars | Cold War Vietnam War Yom Kippur War Iran–Iraq War Persian Gulf War Kosovo War Iraq War First Libyan Civil War[source] | — |
|---|
| Manufacturer | Raytheon Missile Systems Raytheon[source] | China Airborne Missile Academy (CAMA)[source] |
|---|
| Unit cost | US$ 17,000 to $110,000, depending on variant[source] | — |
|---|
| No. built | >70,000[source] | — |
|---|
| Warhead | 126 lb (57 kg) WDU-20/B shaped-charge (A/B/C/D/H models) 300 lb (140 kg) WDU-24/B penetrating blast-fragmentation (E/F/G/J/K models) E models utilize FMU-135/B delayed impact fuze[source] | — |
|---|
| Engine | A/B: Thiokol SR109-TC-1 D/E/F/G/H/J/K: SR114-TC-1 (or Aerojet SR115-AJ-1) solid propellant rocket motor via a WPU-4/B or WPU-8/B propulsion section[source] | Dual-pulsed solid-propellant rocket[source] |
|---|
| Propellant | Solid propellant[source] | — |
|---|
| Guidance system | A/B/H/J/K: Contrast seeker D/F/G: imaging infrared guidance E/E2/L: Laser guidance[source] | Active radar homing[source] |
|---|
| Launch platform | — | J-20 , J-35 , J-10C , J-15T , J-16 , J-11BG , JF-17 Block-3[source] |
|---|