FORCETALLY
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At a glance
CAMM (missile family)larger figure on 0 of 1
David's Slinglarger 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
CAMM: Missile
Single sourceLaunch canister
Single sourceConfiguration
| Specification | CAMM (missile family) | David's Sling |
|---|---|---|
| Type | Anti-aircraft and anti-missile missile[source] | Medium to long range surface-to-air / anti-ballistic missile[source] |
| Place of origin | United Kingdom United Kingdom & Italy (CAMM-ER) United Kingdom & Poland (CAMM-MR)[source] | Israel United States[source] |
| In service | Royal Navy – 2018 Royal New Zealand Navy – 2020 British Army – 2021 Chilean Navy – 2022 Brazilian Navy – 2025[source] | Israel Defense Forces (2017–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]
est without booster est
Single sourcewith booster
Single sourceest. 3.38 m (11 ft 1 in) without booster est. 4.95 m (16 ft 3 in) with booster[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]
booster
Single sourceest missile est
Single sourceCAMM: Missile
Single sourceIn a launch canister
Single sourceIn a launch canister CAMM-ER: Missile
Single sourceMass
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]
Maximum; Maximum speed
Single sourceMaximum; Mach 3 (
Single sourceMach 3 (1,029 m/s; 3,376 ft/s)[source]
Maximum; Maximum speed
Single sourceMaximum; est. Mach 4 – Mach 5.5 (
Single sourceOperational; CAMM: > CAMM-ER: >
Single sourceOperational; CAMM-MR: >
Single sourceOperational; Operational range
Single sourceCAMM: > 25 km (16 mi) CAMM-ER: > 45 km (28 mi) CAMM-MR: > 100 km (62 mi)[source]
Operational; against ballistic targets
Single sourceOperational; est against aerial targets est
Single sourceWarhead 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.
| — |
| Designer | MBDA UK MBDA (CAMM-ER)[source] | Rafael Advanced Defense Systems and Raytheon Missiles & Defense[source] |
|---|
| Designed | 2004[source] | 2009–present[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] | AESA MMW 3D Radar Dual Electro-optical FPA CCD + IIR Seeker Asymmetric 360° Multi-Seeker assembly 3-way Datalink with real time automatic and manual retargeting ECCM + IRCCM[source] |
|---|
| Steering system | Four folding cruciform wings[source] | Supermaneuverable Asymmetric Kill Vehicle[source] |
|---|
| References | Janes[source] | Janes[source] |
|---|
| Manufacturer | MBDA[source] | Rafael and Raytheon[source] |
|---|
| Unit cost | — | US$700,000[source] |
|---|
| Produced | — | 2017–present[source] |
|---|
| Detonation mechanism | — | Kinetic Hit-to-kill[source] |
|---|
| Propellant | — | Two-stage Solid[source] |
|---|
| Reported operators | — |
|
|---|
est. 230 mm (9 in) missile est. 305 mm (12 in) booster[source]
est. Mach 4 – Mach 5.5 (1,400–1,870 m/s; 4,500–6,140 ft/s)[source]
est. 180 km (110 mi) against aerial targets est. 75 km (47 mi) against ballistic targets[source]