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 3 of 3
J-600T Yıldırımlarger figure on 0 of 3
Measured figures
Length
Single source8.77 m (28.8 ft)[source]
Length
Single sourceConfiguration
| Specification | Hwasong-11A | J-600T Yıldırım |
|---|---|---|
| Speed | — | Supersonic[source] |
| Type | Short-range ballistic missile[source] | Theater ballistic missile Short-range ballistic missile[source] |
| Place of origin | North Korea[source] | Turkey[source] |
| In service | 2019–present[source] | 2001 – present[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
6.10 m[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Used by |
|---|
North Korea ( Korean People's Army Strategic Force ) Russia[source] |
Turkish Army[source] |
| Wars | Russo-Ukrainian war[source] | — |
|---|
| Designed | 2018[source] | — |
|---|
| Manufacturer | February 11 Plant[source] | Roketsan[source] |
|---|
| Developed into | See § Variants[source] | — |
|---|
| Warhead | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] | 480 kg TNT + RDX conventional warhead[source] |
|---|
| Engine | Solid-fueled engine[source] | Single-stage solid propellant[source] |
|---|
| Propellant | Solid composite[source] | HTPB -based composite solid propellant[source] |
|---|
| Flight altitude | 50–60 km (31–37 mi)[source] | — |
|---|
| Guidance system | Inertial navigation system (INS), possible satellite navigation[source] | Inertial and Optical guidance systems[source] |
|---|
| Accuracy | 35–200 m (115–656 ft)[source] | — |
|---|
| Launch platform | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] | F-600T (based on MAN 26.372 6x6)[source] |
|---|
| Designer | — | Roketsan[source] |
|---|
| Produced | — | 1998[source] |
|---|
| Detonation mechanism | — | Proximity / Impact[source] |
|---|
| J-600T Yıldırım I | — | SRBM (150 km range)[source] |
|---|
| J-600T Yıldırım II | — | SRBM (300 km range)[source] |
|---|
| J-600T Yıldırım III | — | SRBM (900 km range)[source] |
|---|