FORCETALLY
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At a glance
Ghauri-IIlarger figure on 3 of 3
Measured figures
Length
Single source26 m (85 ft)[source]
Length
Single sourceConfiguration
| Specification | Ghauri-II | Hwasong-11A |
|---|---|---|
| Type | MRBM[source] | Short-range ballistic missile[source] |
| Place of origin | Pakistan[source] | North Korea[source] |
| In service | 2004–present (Not currently deployed)[source] | 2019–present[source] |
| Used by | Pakistan Army ( Army Strategic Forces Command )[source] | North Korea ( Korean People's Army Strategic Force ) Russia |
Hwasong-11Alarger figure on 0 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
8.77 m (28.8 ft)[source]
Mass
Single source3,415–8,729 kg (7,529–19,244 lb)[source]
Warhead weight
Single source1,500 kg (3,300 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Khan Research Laboratories (KRL)[source] | — |
|---|
| Designed | 1993–2003[source] | 2018[source] |
|---|
| Manufacturer | Khan Research Laboratories[source] | February 11 Plant[source] |
|---|
| Variants | Ghauri-III[source] | — |
|---|
| Warhead | HE / NE[source] | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] |
|---|
| Engine | Two-stage[source] | Solid-fueled engine[source] |
|---|
| Transmission | Manual[source] | — |
|---|
| Suspension | Atego x 8WD semi-trailer[source] | — |
|---|
| Propellant | Liquid-propellant[source] | Solid composite[source] |
|---|
| Flight altitude | 612 mi (985 km), reached in first test flight[source] | 50–60 km (31–37 mi)[source] |
|---|
| Guidance system | Inertial , Terminal[source] | Inertial navigation system (INS), possible satellite navigation[source] |
|---|
| Launch platform | Launch pad[source] | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] |
|---|
| Wars | — | Russo-Ukrainian war[source] |
|---|
| Developed into | — | See § Variants[source] |
|---|
| Accuracy | — | 35–200 m (115–656 ft)[source] |
|---|