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At a glance
2K11 Kruglarger 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
Length
Single sourcewith missiles
Single sourceConfiguration
| Specification | 2K11 Krug | David's Sling |
|---|---|---|
| Type | Transportable SAM system[source] | Medium to long range surface-to-air / anti-ballistic missile[source] |
| Place of origin | Soviet Union[source] | Israel United States[source] |
| In service | 1965–present 1965–1990s (USSR)[source] | Israel Defense Forces (2017–present)[source] |
| Used by | See list of operators[source] | — |
7.5 m (25 ft) (9.46 m (31 ft) with missiles)[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]
booster
Single sourceest missile est
Single sourceest. 460 mm (18 in) missile est. 480 mm (19 in) booster[source]
with missiles
Single source4.472 m (14 ft 8 in) (with missiles)[source]
V59 V-12 water-cooled diesel
Single sourceV59 V-12 water-cooled diesel 520 hp[source]
Warhead weight
Single source150 kg (330 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer |
|---|
Lyulev Novator[source] |
Rafael Advanced Defense Systems and Raytheon Missiles & Defense[source] |
| Designed | 1957[source] | 2009–present[source] |
|---|
| Manufacturer | MZiK[source] | Rafael and Raytheon[source] |
|---|
| Variants | Krug, Krug-A, Krug-M, Krug-M1, Krug-M2, Krug-M3[source] | — |
|---|
| Armour | 15 mm (0.59 in)[source] | — |
|---|
| Power/weight | 17.33 hp/t[source] | — |
|---|
| Ground clearance | 0.44 m (1 ft 5 in)[source] | — |
|---|
| Fuel capacity | 850 L (190 imp gal; 220 US gal)[source] | — |
|---|
| Warhead | Frag-HE[source] | — |
|---|
| Detonation mechanism | contact and proximity fuzes[source] | Kinetic Hit-to-kill[source] |
|---|
| Propellant | kerosene fuelled ramjet[source] | Two-stage Solid[source] |
|---|
| Flight altitude | 24,500 metres (80,400 ft)[source] | — |
|---|
| Boost time | four solid fuel booster rocket motors[source] | — |
|---|
| Guidance system | Radio command[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] |
|---|
| Unit cost | — | US$700,000[source] |
|---|
| Produced | — | 2017–present[source] |
|---|
| Steering system | — | Supermaneuverable Asymmetric Kill Vehicle[source] |
|---|
| References | — | Janes[source] |
|---|
| Reported operators |
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