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At a glance
Measured figures
PL-15E
Single source20.3 cm (8.0 in) (PL-15E)[source]
CM-501G
Single sourceCM-501GA
Single sourceCM-501X
Single sourceCM-501XA
Single sourceCM-502
Single sourceCM-501G: 150 kg (330 lb) CM-501GA: 100 kg (220 lb) CM-501X: 170 kg (370 lb) CM-501XA: 100 kg (220 lb) CM-502: 45 kg (99 lb)[source]
(PL-15) ≤
Single sourcePL-15E
Single source200–230 kg (441–507 lb) (PL-15) ≤210 kg (463 lb) (PL-15E)[source]
Operational; CM-5012
Single sourceOperational; CM-501G
Single sourceOperational; CM-501GA
Single sourceOperational; CM-501X/XA
Single sourceCM-501G: 70 km (43 mi) CM-501GA: 40 km (25 mi) CM-501X/XA: 70 km (43 mi) CM-5012: 25 km (16 mi)[source]
Operational; PL-15
Single sourceOperational; PL-15E
Single source150–200 km (93–124 mi) (PL-15) 145 km (90 mi) (PL-15E)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | CM-501 | PL-15 |
|---|---|---|
| Speed | CM-502: Mach 1.1[source] | Mach 5+[source] |
| Type | anti-ship , anti-tank , land-attack missile / loitering munition[source] | Beyond-visual-range air-to-air missile[source] |
| Place of origin | China[source] | People's Republic of China[source] |
| In service | 2019-present[source] | 2016–present[source] |
| Used by | People's Liberation Army[source] | People's Liberation Army Air Force[source]Operator listed in the retained article; inventory date not specified 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 | China Aerospace Science and Industry Corporation (CASIC)[source] | China Airborne Missile Academy (CAMA)[source] |
| Unit cost | depends on models[source] | — |
| Produced | 2010s-present[source] | — |
| Warhead | CM-501G: 40 kg (88 lb) HE CM-501GA: 20 kg (44 lb) HE CM-501X: 20 kg (44 lb) HE CM-501XA: 8.5 kg (19 lb) HE CM-502: 11 kg (24 lb) HE/SAP-HE[source] | — |
| Detonation mechanism | Impact / Proximity / Semi-armor-piercing[source] | — |
| Engine | CM-501G/GA/CM-502: solid-fuel rocket CM-501X/XA: turbojet with rocket booster[source] | Dual-pulsed solid-propellant rocket[source] |
| Propellant | solid fuel[source] | — |
| Guidance system | All variant: Datalink + Satellite + INS CM-501G: Combined IIR , SAL CM-501GA: Combined IIR , TV CM-501X/XA: TV / IIR / passive radar / combined IIR with mmW CM-502: TV/ IIR /SAL[source] | Active radar homing[source] |
| Launch platform | Air-launched, vertical launch system on ground, naval vehicles.[source] | J-20 , J-35 , J-10C , J-15T , J-16 , J-11BG , JF-17 Block-3[source] |
| Reported operators |
| — |