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ForceTally · AI-generated illustration · Not a photograph · AI-generated · OpenAI output terms · Source ↗ · Modified
FORCETALLY
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At a glance
AGM-65 Mavericklarger figure on 1 of 1
K-13 (missile)larger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source249 cm (8 ft 2 in)[source]
R-13M
Single sourceConfiguration
| Specification | AGM-65 Maverick | K-13 (missile) |
|---|---|---|
| Type | Air-to-surface missile[source] | Short-range infrared homing air-to-air missile[source] |
| Place of origin | United States[source] | Soviet Union[source] |
| In service | 30 August 1972 – present[source] | 1961[source] |
| Used by | >30 countries[source] | See Operators |
R-3R
Single source2.830 m (9 ft 3.4 in) (R-13M) 3.48 m (11 ft 5 in) (R-3R)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| 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] | Vympel[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] | 7.4 kg (16 lb)[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] | solid-fuel rocket engine[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] | infrared homing[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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|---|