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.
At a glance
Hwasong-11Alarger figure on 1 of 4
Shaurya (missile)larger figure on 3 of 4
Measured figures
Length
Single source8.77 m (28.8 ft)[source]
Length
Single sourceConfiguration
| Specification | Hwasong-11A | Shaurya (missile) |
|---|---|---|
| Type | Short-range ballistic missile[source] | Short-range ballistic missile[source] |
| Place of origin | North Korea[source] | India[source] |
| In service | 2019–present[source] | — |
| Used by | North Korea ( Korean People's Army Strategic Force ) Russia[source] | Strategic Forces Command[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
10 m (33 ft )[source]
Maximum; 2.55 km/s
Single sourceMaximum; Mach 7.5 (
Single sourceMach 7.5 (9,190 km/h; 5,710 mph; 2.55 km/s)[source]
Warhead weight
Single source200–1,000 kilograms (440–2,200 lb)[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] | Bharat Dynamics Limited[source] |
|---|
| Developed into | See § Variants[source] | — |
|---|
| Warhead | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] | Conventional and strategic nuclear weapon[source] |
|---|
| Engine | Solid-fueled engine[source] | Two-stage solid rocket motor[source] |
|---|
| Propellant | Solid composite[source] | Solid fuel[source] |
|---|
| Flight altitude | 50–60 km (31–37 mi)[source] | 50 km (31 mi)[source] |
|---|
| Guidance system | Inertial navigation system (INS), possible satellite navigation[source] | RLG - INS and accelerometer[source] |
|---|
| Accuracy | 35–200 m (115–656 ft)[source] | 20 m to 30 m CEP[source] |
|---|
| Launch platform | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] | Canisterised transporter erector launcher or underground silo[source] |
|---|
| Designer | — | Research Centre Imarat[source] |
|---|
| Produced | — | 2011–present[source] |
|---|
| Reported operators | — |
|
|---|