FORCETALLY
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Measured figures
est without booster est
Single sourcewith booster
Single sourceConfiguration
| Specification | David's Sling | DK-10 |
|---|---|---|
| Type | Medium to long range surface-to-air / anti-ballistic missile[source] | Medium range surface-to-air missile[source] |
| Place of origin | Israel United States[source] | China[source] |
| In service | Israel Defense Forces (2017–present)[source] | 2017 – present[source] |
| Designer | Rafael Advanced Defense Systems and Raytheon Missiles & Defense[source] | — |
est. 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. 230 mm (9 in) missile est. 305 mm (12 in) booster[source]
Diameter · source measurement 1
Single sourceDiameter · source measurement 2
Single source203 / 260 mm
Maximum; est. Mach 4 – Mach 5.5 (
Single sourceMaximum; Maximum speed
Single sourceest. Mach 4 – Mach 5.5 (1,400–1,870 m/s; 4,500–6,140 ft/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designed | 2009–present[source] | — |
|---|
| Manufacturer | Rafael and Raytheon[source] | Aviation Industry Corporation of China (AVIC) China North Industries Corporation[source] |
|---|
| Unit cost | US$700,000[source] | — |
|---|
| Produced | 2017–present[source] | — |
|---|
| Detonation mechanism | Kinetic Hit-to-kill[source] | impact / proximity[source] |
|---|
| Propellant | Two-stage Solid[source] | solid fuel[source] |
|---|
| Guidance system | 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] | inertial navigation system / datalink / ARH[source] |
|---|
| Steering system | Supermaneuverable Asymmetric Kill Vehicle[source] | — |
|---|
| References | Janes[source] | — |
|---|
| Used by | — | Royal Moroccan Army Rwanda Defence Force[source] |
|---|
| Warhead | — | 20 kg HE warhead[source] |
|---|
| Engine | — | rocket motor[source] |
|---|
| Flight altitude | — | 30 m to 20 km[source] |
|---|
| Launch platform | — | Surface[source] |
|---|
| Reported operators |
| — |
|---|