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At a glance
Measured figures
R-13M
Single source631 mm (24.8 in) (R-13M)[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]
R-13M
Single source90 kg (200 lb) (R-13M)[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; Operational range
Single sourceR-3S / R-3R · effective
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | CM-501 | K-13 (missile) |
|---|---|---|
| Type | anti-ship , anti-tank , land-attack missile / loitering munition[source] | Short-range infrared homing air-to-air missile[source] |
| Place of origin | China[source] | Soviet Union[source] |
| In service | 2019-present[source] | 1961[source] |
| Used by | People's Liberation Army[source] | See Operators[source] |
| Manufacturer | China Aerospace Science and Industry Corporation (CASIC)[source] | Vympel[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] | 7.4 kg (16 lb)[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] | solid-fuel rocket engine[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] | infrared homing[source] |
| Launch platform | Air-launched, vertical launch system on ground, naval vehicles.[source] | MiG-21 , MiG-23 , MiG-19 , MiG-17 Sukhoi Su-17/20/22[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 |
|
|
R-3S / R-3R · max
Single source