FORCETALLY
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Measured figures
Mass
Single source3,415–8,729 kg (7,529–19,244 lb)[source]
Hwasong-11A / KN-23 only · Range
Single sourceHwasong-11B / KN-24 only · Range
Single sourceKN-10 upgraded version only · Range
Single sourceOriginal Hwasong-11 / KN-02 only · Range
Single source120–170 km (75–106 mi)[source]Original Hwasong-11 / KN-02 only
220 km (140 mi)[source]KN-10 upgraded version only
900 km (560 mi)[source]Hwasong-11A / KN-23 only
410 km (250 mi)[source]Hwasong-11B / KN-24 only
Operational; Operational range
Single source190–900 km (120–560 mi)[source]
Hwasong-11A / KN-23 at stated 690 km configuration · Warhead mass
Single sourceOriginal Hwasong-11 / KN-02 alternative warheads · or
Single sourceOriginal Hwasong-11 / KN-02 alternative warheads · Warhead mass
Single source250 kg (550 lb) or 485 kg (1,069 lb)[source]Original Hwasong-11 / KN-02 alternative warheads
500 kg (1,100 lb)[source]Hwasong-11A / KN-23 at stated 690 km configuration
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Hwasong-11 | Hwasong-11A |
|---|---|---|
| Type | single-stage, solid-fueled, short-range ballistic missile[source] | Short-range ballistic missile[source] |
| National origin | North Korea[source] | — |
| Manufacturer | February 11 Plant, part of the Ryongsong Machine Complex[source] | February 11 Plant[source] |
| Propulsion | single-stage, solid-fueled[source] | — |
| Place of origin | — | North Korea[source] |
| In service | — | 2019–present[source] |
| Used by | — | North Korea ( Korean People's Army Strategic Force ) Russia[source] |
| Wars | — | Russo-Ukrainian war[source] |
| Designed | — | 2018[source] |
| Developed into | — | See § Variants[source] |
| Warhead | — | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] |
| Engine | — | Solid-fueled engine[source] |
| Propellant | — | Solid composite[source] |
| Flight altitude | — | 50–60 km (31–37 mi)[source] |
| Guidance system | — | Inertial navigation system (INS), possible satellite navigation[source] |
| Accuracy | — | 35–200 m (115–656 ft)[source] |
| Launch platform | — | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] |