Armement Air-Sol Modulaire vs Zuni (rocket)

FORCETALLY

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AMissiles

Armement Air-Sol Modulaire

Glide bomb Air-to-surface missile

BMissiles

Zuni (rocket)

Air-to-surface rocket

First system

Second system

At a glance

Side by side

Length comparisonOne shared metre scale

Armement Air-Sol ModulaireLength

3.1 m

Length source ↗

Zuni (rocket)Length

2 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Armement Air-Sol Modulairelarger figure on 1 of 1

Length+55%

Zuni (rocket)larger figure on 0 of 1

None

Counts only measures both sources give with the same scope. A larger figure is not a better system.

Measured figures

Head to head

9 of 26 rows sourced on both sides

3.1m

Length+55%

All recorded figures & sources

3.1 m

Length

Single source

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

2 m

Length

Single source

Configuration

Details

Armement Air-Sol Modulaire and Zuni (rocket) configuration
Specification	Armement Air-Sol Modulaire	Zuni (rocket)
Type	Glide bomb Air-to-surface missile^[source]	Air-to-surface rocket^[source]
Place of origin	France^[source]	United States^[source]
In service	2007–present^[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]	United States military French 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]	—

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]	various^[source]

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

Guidance system	Hybrid inertial / GPS in decametric all-weather version Hybrid inertial/GPS + infrared homing or SALH in metric day/night version^[source]	None^[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]	—

Produced	—	1957–present^[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	—