CAMPEM
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| CAMPEM | |
|---|---|
| Type | Anti-radiation missile |
| Place of origin |  Sieuxerr |
| Service history | |
| In service | 1995-Present |
| Used by | Sieuxerr |
| Production history | |
| Designer | Aérospatiale-Matra |
| Designed | 1994 |
| Manufacturer | Aérospatiale-Matra |
| Produced | 1995 |
| Specifications | |
| Weight | 410 kg |
| Length | 4.7 m |
| Diameter | 290 mm |
| Warhead | Annular blast-fragmenting warhead |
| Warhead weight | 100 kg |
Detonation mechanism | Proximity fuze |
| Engine | 2 stage rocket |
| Wingspan | 800 mm |
| Propellant | Solid fuel |
Operational range | 110 km |
| Speed | Mach 3.1 |
Guidance system | Passive radar homing, GPS, home-on-jam, active radar guidance |
Launch platform | Aircraft |
The Contre rAyonneMent Précision flânagE Missiles is a Sieuxerrian designed anti-radiation missile designed to engage land, and later with upgrade packages, allowed the engagement of aircraft such as AWACS and C4I aircraft. Used typically by the MB.4000N/D aircraft when conducting Suppression of Enemy Air Defenses operations.