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At a glance
Hwasong-11Alarger figure on 0 of 4
RT-2PM2 Topol-Mlarger figure on 4 of 4
Measured figures
Length
Single source8.77 m (28.8 ft)[source]
Length
Single sourceConfiguration
| Specification | Hwasong-11A | RT-2PM2 Topol-M |
|---|---|---|
| Type | Short-range ballistic missile[source] | Intercontinental ballistic missile[source] |
| Place of origin | North Korea[source] | Russia[source] |
| In service | 2019–present[source] | December 2000–present[source] |
| Used by | North Korea ( Korean People's Army Strategic Force ) Russia[source] | Russian Strategic Rocket Forces |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
22.7 m (74 ft)[source]
Maximum; Mach 22
Single sourceMaximum; Maximum speed · source measurement 1
Single sourceMaximum; Maximum speed · source measurement 2
Single source7,520 metres per second (27,100 km/h; 16,800 mph; Mach 22)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Russo-Ukrainian war[source] | — |
|---|
| Designed | 2018[source] | — |
|---|
| Manufacturer | February 11 Plant[source] | Votkinsk Machine Building Plant[source] |
|---|
| Developed into | See § Variants[source] | — |
|---|
| Warhead | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] | 1 x 1.0 Mt[source] |
|---|
| Engine | Solid-fueled engine[source] | Three-stage Solid-fuel rocket[source] |
|---|
| Propellant | Solid composite[source] | — |
|---|
| Flight altitude | 50–60 km (31–37 mi)[source] | — |
|---|
| Guidance system | Inertial navigation system (INS), possible satellite navigation[source] | Inertial with GLONASS[source] |
|---|
| Accuracy | 35–200 m (115–656 ft)[source] | 200 m CEP[source] |
|---|
| Launch platform | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] | Silo, road-mobile TEL[source] |
|---|
| Designer | — | Moscow Institute of Thermal Technology[source] |
|---|
| Produced | — | December 1994–2010[source] |
|---|