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ForceTally · AI-generated illustration · Not a photograph · AI-generated · OpenAI output terms · Source ↗ · Modified
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At a glance
Hwasong-11Alarger figure on 1 of 1
Kh-47M2 Kinzhallarger figure on 0 of 1
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]
estimated
Single sourceConfiguration
| Specification | Hwasong-11A | Kh-47M2 Kinzhal |
|---|---|---|
| Type | Short-range ballistic missile[source] | Air-launched ballistic missile[source] |
| Place of origin | North Korea[source] | Russia[source] |
| In service | 2019–present[source] | 2017–present[source] |
| Used by | North Korea ( Korean People's Army Strategic Force ) Russia[source] | Russian Aerospace Forces |
7.2 m (23 ft 7 in) (estimated)[source]
Maximum; Maximum speed
Single sourceMaximum; Up to Mach 10 (
Single sourceUp to Mach 10 (3,400 m/s; 11,200 ft/s)[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] | Russo-Ukrainian war[source] |
|---|
| Designed | 2018[source] | — |
|---|
| Manufacturer | February 11 Plant[source] | KBM[source] |
|---|
| Developed into | See § Variants[source] | — |
|---|
| Warhead | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] | Low yield nuclear warhead (5 to 50 kt ) or conventional HE[source] |
|---|
| Engine | Solid-fueled engine[source] | Solid-propellant rocket motor[source] |
|---|
| Propellant | Solid composite[source] | — |
|---|
| Flight altitude | 50–60 km (31–37 mi)[source] | — |
|---|
| Guidance system | Inertial navigation system (INS), possible satellite navigation[source] | INS , mid-course update[source] |
|---|
| Accuracy | 35–200 m (115–656 ft)[source] | — |
|---|
| Launch platform | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] | MiG-31BM/K Tu-22M3M Su-34 (reportedly) Su‐57 (planned)[source] |
|---|
| Designer | — | Believed to be: Votkinsk Plant State Production Association and Tactical Missiles Corporation JSC[source] |
|---|
| Unit cost | — | US$10 million[source] |
|---|
| Steering system | — | Four cropped delta‐fins[source] |
|---|
| References | — | Janes , CSIS[source] |
|---|