FORCETALLY
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At a glance
CAMM (missile family)larger figure on 1 of 3
Flakpanzer Gepardlarger figure on 2 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
CAMM: Missile
Single sourceLaunch canister
Single sourceConfiguration
| Specification | CAMM (missile family) | Flakpanzer Gepard |
|---|---|---|
| Type | Anti-aircraft and anti-missile missile[source] | Self-propelled anti-aircraft gun[source] |
| Place of origin | United Kingdom United Kingdom & Italy (CAMM-ER) United Kingdom & Poland (CAMM-MR)[source] | Switzerland West Germany[source] |
| In service | Royal Navy – 2018 Royal New Zealand Navy – 2020 British Army – 2021 Chilean Navy – 2022 Brazilian Navy – 2025[source] | 1976–present[source] |
| Wars | Red Sea crisis[source] |
Launch canister CAMM-ER: Missile
Single sourceLength
Single sourceCAMM: Missile: 3.2 m (10 ft 6 in) Launch canister: 3.4 m (11 ft 2 in) CAMM-ER: Missile: 4.2 m (13 ft 9 in) Launch canister: 4.4 m (14 ft 5 in)[source]
Overall
Single sourceOverall: 7.68 m (25 ft 2 in)[source]
Radar retracted
Single sourceRadar retracted: 3.29 m (10 ft 10 in)[source]
CAMM-ER: Missile
Single sourceCAMM: Missile Launch canister (square)
Single sourceDiameter
Single sourceLaunch canister (square)
Single sourceCAMM: Missile: 166 mm (6.5 in) Launch canister (square): 275 mm (10.8 in) CAMM-ER: Missile: 190 mm (7.5 in) Launch canister (square): 275 mm (10.8 in)[source]
Mass
Single sourceCAMM: Missile
Single sourceIn a launch canister
Single sourceIn a launch canister CAMM-ER: Missile
Single sourceCAMM: Missile: 99 kg (218 lb) In a launch canister: 181 kg (399 lb) CAMM-ER: Missile: 166 kg (366 lb) In a launch canister: 250 kg (550 lb)[source]
Mass
Single source47.5 t (46.7 long tons; 52.4 short tons)[source]
driver, gunner, commander
Single source3 (driver, gunner, commander)[source]
10- cylinder , 37,400 cc (2,280 cu in ) MTU multi-fuel engine
Single source10- cylinder , 37,400 cc (2,280 cu in ) MTU multi-fuel engine 830 PS (819 hp, 610 kW)[source]
Warhead weight
Single source10 kg (22 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Russo-Ukrainian War[source] |
| Designer | MBDA UK MBDA (CAMM-ER)[source] | Oerlikon-Bührle AG (Switzerland) Contraves (Switzerland) Siemens-Albis AG (Switzerland) Krauss-Maffei AG (vehicle - West Germany)[source] |
|---|
| Designed | 2004[source] | — |
|---|
| Warhead | High-explosive blast fragmentation warhead with laser proximity and impact fuze[source] | — |
|---|
| Engine | Solid-fuel rocket motor[source] | — |
|---|
| Flight altitude | CAMM & CAMM-ER: 10,000 m (33,000 ft)[source] | — |
|---|
| Guidance system | Inertial guidance system with mid-course update and active radar terminal homing[source] | — |
|---|
| Steering system | Four folding cruciform wings[source] | — |
|---|
| References | Janes[source] | — |
|---|
| Manufacturer | MBDA[source] | Krauss-Maffei AG (licence production)[source] |
|---|
| Used by | — | See Operators[source] |
|---|
| Armor | — | conventional steel[source] |
|---|
| Main armament | — | 2 × 35 mm Oerlikon GDF autocannon , each with 320 rounds anti-air ammunition and 20 rounds anti-tank[source] |
|---|
| Secondary armament | — | 2 × quad 76 mm smoke grenade dischargers[source] |
|---|
| Power/weight | — | 17.5 PS/t[source] |
|---|
| Suspension | — | Torsion bar suspension[source] |
|---|