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At a glance
K-13 (missile)larger figure on 0 of 1
Nimrod (missile)larger figure on 1 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
R-13M
Single sourceR-3R
Single sourceConfiguration
| Specification | K-13 (missile) | Nimrod (missile) |
|---|---|---|
| Type | Short-range infrared homing air-to-air missile[source] | — |
| Place of origin | Soviet Union[source] | — |
| In service | 1961[source] | — |
| Used by | See Operators[source] | — |
| Manufacturer | Vympel[source] | — |
| Warhead | 7.4 kg (16 lb)[source] |
2.830 m (9 ft 3.4 in) (R-13M) 3.48 m (11 ft 5 in) (R-3R)[source]
Length
Single sourceLength : 265 cm[source]Nimrod (missile) · Characteristics · Length : 265 cm
R-13M
Single source631 mm (24.8 in) (R-13M)[source]
Operational; Operational range
Single sourceR-3S / R-3R · effective
Single sourceR-3S / R-3R · max
Single source1.0 to 3.5 kilometres (0.6 to 2.2 mi )[source]
0.9 to 7 km max, 2 km effective[source]
Effective range : 300 - 36,000 meters[source]Nimrod (missile) · Characteristics · Effective range : 300 - 36,000 meters
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Engine | solid-fuel rocket engine[source] | — |
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| Guidance system | infrared homing[source] | — |
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| Launch platform | MiG-21 , MiG-23 , MiG-19 , MiG-17 Sukhoi Su-17/20/22[source] | — |
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| Guidance | (R-3S) infrared homing ; (R-3R) SARH[source] | — |
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| Launch weight | (R-3S) 75 kg (166 lb); (R-3R) 93 kg (205 lb)[source] | — |
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| Explosive content | 5.3 kg (11.68 lbs) of TGAF-5 (40% TNT, 40% RDX, 20% Aluminium powder)[source] | — |
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| Fuze | type 428 proximity fuze and I-107 Contact fuze (R-3R)[source] | — |
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| Former operator · Bulgaria | Bulgaria[source] | — |
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| Former operator · Guinea | Guinea[source] | — |
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| Role | — | long-range air-to-surface missile[source] |
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| Source measurement | — | Nimrod has a semi-active laser guidance system that operates day or night. Its flight trajectory can be set below obscuring cloud layers, while a forward reconnaissance scout team uses a laser designator to direct it from up to 26 km (16 mi).[source]Nimrod (missile) · Lead; only the objects and conditions stated in this passage Nimrod allows a gunner to pre-select a flight trajectory mode. This can be direct trajectory, high cruise trajectory or low cruise trajectory , the cruise altitude being constant and between 300–1,500 m (980–4,920 ft).[source]Nimrod (missile) · Description; only the objects and conditions stated in this passage The gimballed and stabilised seeker head acquires, tracks and homes in on its target using localised proportional navigation. It is said to have a view angle of more than 30°. The seeker has a search area 5 km (3.1 mi) wide and deep. In the terminal flight phase, the weapon adopts a dive angle of approximately 45° to strike an armoured target on the thinner, more vulnerable upper surfaces.[source]Nimrod (missile) · Description; only the objects and conditions stated in this passage The missile is stored in a sealed canister which also acts as the launcher. Total weight of the missile and canister is 150 kg (330 lb). It has five main sections: seeker, guidance and control, warhead, solid-propellant rocket motor, and servo. It is roll-stabilised in flight. Time to come into action at a launch site is less than 3 minutes; there is no need to survey the site for alignment or levelling, nor does it require a direct line of sight to a target. The weapon can be fired in single-round, ripple, or salvo modes.[source]Nimrod (missile) · Description; only the objects and conditions stated in this passage Effective range : 300 - 36,000 meters[source]Nimrod (missile) · Characteristics; only the objects and conditions stated in this passage Length : 265 cm[source]Nimrod (missile) · Characteristics; only the objects and conditions stated in this passage Diameter : 17 cm[source]Nimrod (missile) · Characteristics; only the objects and conditions stated in this passage Body : 18 cm[source]Nimrod (missile) · Characteristics; only the objects and conditions stated in this passage Span 40 cm[source]Nimrod (missile) · Characteristics; only the objects and conditions stated in this passage Weight : 100 kg[source]Nimrod (missile) · Characteristics; only the objects and conditions stated in this passage Speed : ~1000 km/h or Mach 0.8[source]Nimrod (missile) · Characteristics; only the objects and conditions stated in this passage Nimrod 2 – A dual guidance, laser and Global Positioning System (GPS), homing missile, with a range of 26 km (16 mi), and a mobile launcher. The warhead is 14 kg (31 lb), and the missile supports various warheads for a variety of targets. This missile is well suited to rapid response and for coastal defence.[source]Nimrod (missile) · Variants; only the objects and conditions stated in this passage Nimrod 3 – An extended variant of Nimrod 2. The missile has a range of 50 km (31 mi) with 50 kg (110 lb) warhead. It supports various warheads for a wide range of targets, and has a mobile launcher.[source]Nimrod (missile) · Variants; only the objects and conditions stated in this passage Nimrod SR – A short-range (8 km (5.0 mi)) variant that can be fired from ground and airborne platforms.[source]Nimrod (missile) · Variants; only the objects and conditions stated in this passage |
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| Country of origin | — | Israel[source]Inventory Origin column; table 4, row 5, cell 2; revision 1349150138; retrieved 2026-10-02 |
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