AI-generated illustration · Not a photograph
Credit
ForceTally · AI-generated illustration · Not a photograph · AI-generated · OpenAI output terms · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
BBallistic missiles
Rocket artillery Short-range ballistic missile Medium-range ballistic missile Anti-ship ballistic missile
At a glance
Hwasong-11Alarger figure on 2 of 2
Precision Strike Missilelarger figure on 0 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source8.77 m (28.8 ft)[source]
Length
Single sourceConfiguration
| Specification | Hwasong-11A | Precision Strike Missile |
|---|---|---|
| Type | Short-range ballistic missile[source] | Rocket artillery Short-range ballistic missile Medium-range ballistic missile Anti-ship ballistic missile[source] |
| Place of origin | North Korea[source] | United States[source] |
| In service | 2019–present[source] | 2023–present[source] |
| Used by | North Korea ( Korean People's Army Strategic Force ) Russia[source] |
13 ft (4.0 m)[source]
Warhead weight
Single source200 lb (91 kg)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
United States Australia[source] |
| Wars | Russo-Ukrainian war[source] | 2026 Iran war[source] |
|---|
| Designed | 2018[source] | — |
|---|
| Manufacturer | February 11 Plant[source] | Lockheed Martin Missiles and Fire Control[source] |
|---|
| Developed into | See § Variants[source] | — |
|---|
| Warhead | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] | HE fragmentation blast Unknown number of submunitions Future iterations will possibly include Coyote drones and Hatchet miniature glide bombs from Northrop Grumman .[source] |
|---|
| Engine | Solid-fueled engine[source] | — |
|---|
| Propellant | Solid composite[source] | solid-propellant rocket[source] |
|---|
| Flight altitude | 50–60 km (31–37 mi)[source] | — |
|---|
| Guidance system | Inertial navigation system (INS), possible satellite navigation[source] | Base: INS + GPS Land-based anti-ship missile: Base + anti-radiation seeker + Imaging Infrared (IIR)[source] |
|---|
| Accuracy | 35–200 m (115–656 ft)[source] | — |
|---|
| Launch platform | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] | M270 MLRS , M142 HIMARS , GMARS[source] |
|---|
| Designer | — | Lockheed Martin Missiles and Fire Control[source] |
|---|
| Unit cost | — | < $3.5 million (Increment One)[source] |
|---|
| Launch platforms | — | M270A2 Multiple Launch Rocket System and the M142 High Mobility Artillery Rocket System[source]Unspecified by source |
|---|
| Reported operators | — |
|
|---|