Armement Air-Sol Modulaire vs K-13 (missile)

FORCETALLY

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AMissiles

Armement Air-Sol Modulaire

Glide bomb Air-to-surface missile

BMissiles

K-13 (missile)

Short-range infrared homing air-to-air missile

Credit

cliff1066 · CC BY 2.0 · Resized · CC BY 2.0 · Source ↗ · Modified

First system

Second system

At a glance

Side by side

Length comparisonOne shared metre scale

Armement Air-Sol ModulaireLength

3.1 m

Length source ↗

K-13 (missile)R-3R

3.48 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Measured figures

Head to head

12 of 43 rows sourced on both sides

3.1m

3.48mR-3R

Length

All recorded figures & sources

3.1 m

Length

Single source

3.1 m (10 ft 2 in)^[source]

2.83 m

R-13M

Single source

Configuration

Details

Armement Air-Sol Modulaire and K-13 (missile) configuration
Specification	Armement Air-Sol Modulaire	K-13 (missile)
Type	Glide bomb Air-to-surface missile^[source]	Short-range infrared homing air-to-air missile^[source]
Place of origin	France^[source]	Soviet Union^[source]
In service	2007–present^[source]	1961^[source]
Used by	French Air and Space Force French Naval Aviation Royal Moroccan Air Force Egyptian Air Force Qatar Air Force Indian Air Force Ukrainian Air Force^[source]

Wars	War in Afghanistan First Libyan civil war Mali War Operation Inherent Resolve Russo-Ukrainian War 2025 India–Pakistan conflict^[source]	—

Manufacturer	Safran Electronics & Defense Bharat Electronics^[source]	Vympel^[source]

Unit cost	€ 164,000 (US$210,707) (FY2011) € 252,000 (US$323,770) including development costs (FY2011)^[source]	—

Warhead	250 kg (550 lb) bomb body ( Mk82 , BLU 111 or CBEMS/BANG)^[source]	7.4 kg (16 lb)^[source]

Engine	Solid rocket motor^[source]	solid-fuel rocket engine^[source]

Guidance system	Hybrid inertial / GPS in decametric all-weather version Hybrid inertial/GPS + infrared homing or SALH in metric day/night version^[source]	infrared homing^[source]

Accuracy	10 m (32 ft 10 in) CEP decametric version 1 m (3 ft 3 in) CEP metric version^[source]	—

Launch platform	Dassault Rafale Dassault Mirage 2000D Dassault Mirage F1 F-16 Tejas MiG-29 Su-25 Su-27^[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	Reported operator · France Reported operator · Croatia Reported operator · Egypt Reported operator · India Reported operator · Indonesia Reported operator · Morocco Reported operator · Qatar Reported operator · Ukraine	Reported operator · Angola Reported operator · Bulgaria Reported operator · Congo Reported operator · Cuba Reported operator · Ethiopia Reported operator · Guinea Reported operator · Libya Reported operator · Nigeria Reported operator · North Korea Reported operator · Peru Reported operator · Sudan