Credit
Srđan Popović · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Length
Single source2,720 mm[source]
R-13M
Single sourceConfiguration
| Specification | ALAS (missile) | K-13 (missile) |
|---|---|---|
| Type | Multi-purpose surface-to surface missile[source] | Short-range infrared homing air-to-air missile[source] |
| Place of origin | Serbia[source] | Soviet Union[source] |
| Manufacturer | EDePro , Yugoimport SDPR[source] | Vympel[source] |
| Engine | solid fuel boost phase motor, EDePro TMM-404 single-shaft turbojet[source] | solid-fuel rocket engine |
R-3R
Single source2.830 m (9 ft 3.4 in) (R-13M) 3.48 m (11 ft 5 in) (R-3R)[source]
Warhead weight
Single source10.5 kg[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Guidance system | optical IR or TV[source] | infrared homing[source] |
|---|
| Accuracy | less than 1 meter CEP[source] | — |
|---|
| In service | — | 1961[source] |
|---|
| Used by | — | See Operators[source] |
|---|
| Warhead | — | 7.4 kg (16 lb)[source] |
|---|
| Launch platform | — | 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 |
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