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At a glance
Abdali-Ilarger figure on 1 of 3
Hwasong-11Alarger figure on 2 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source9.75 m (384 in)[source]
Length
Single sourceConfiguration
| Specification | Abdali-I | Hwasong-11A |
|---|---|---|
| Type | SRBM[source] | Short-range ballistic missile[source] |
| Place of origin | Pakistan[source] | North Korea[source] |
| Used by | Pakistan Army Army Strategic Forces Command[source] | North Korea ( Korean People's Army Strategic Force ) Russia[source] |
| Designer | SUPARCO (Rocket stage) DESTO (Warhead design/assembly)[source] | — |
8.77 m (28.8 ft)[source]
Warhead weight
Single source500 kg (1,100 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designed | 1993–97[source] | 2018[source] |
|---|
| Manufacturer | SUPARCO[source] | February 11 Plant[source] |
|---|
| Warhead | Single conventional HE / ICM[source] | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] |
|---|
| Transmission | Automatic[source] | — |
|---|
| Suspension | MAZ-7310 8WD (With Pakistani military markings)[source] | — |
|---|
| Propellant | Solid-propellent[source] | Solid composite[source] |
|---|
| Guidance system | Inertial , Terminal[source] | Inertial navigation system (INS), possible satellite navigation[source] |
|---|
| Accuracy | 100 m (330 ft)—150 m (490 ft) CEP .[source] | 35–200 m (115–656 ft)[source] |
|---|
| Launch platform | Transporter erector launcher (TEL)[source] | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] |
|---|
| In service | — | 2019–present[source] |
|---|
| Wars | — | Russo-Ukrainian war[source] |
|---|
| Developed into | — | See § Variants[source] |
|---|
| Engine | — | Solid-fueled engine[source] |
|---|
| Flight altitude | — | 50–60 km (31–37 mi)[source] |
|---|