FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Ghauri (missile)larger figure on 4 of 4
Hwasong-11Alarger figure on 0 of 4
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source15.90 m (52.2 ft)[source]
Length
Single sourceConfiguration
| Specification | Ghauri (missile) | Hwasong-11A |
|---|---|---|
| Type | MRBM[source] | Short-range ballistic missile[source] |
| Place of origin | Pakistan[source] | North Korea[source] |
| In service | 2003 –present[source] | 2019–present[source] |
| Used by | Pakistan Army ( Army Strategic Forces Command )[source] | North Korea ( Korean People's Army Strategic Force ) Russia |
8.77 m (28.8 ft)[source]
Warhead weight
Single source750 kg (1,650 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 | 1994–2001[source] | 2018[source] |
|---|
| Manufacturer | Khan Research Laboratories[source] | February 11 Plant[source] |
|---|
| No. built | 30 (estimated 2021)[source] | — |
|---|
| Variants | Ghauri-II , Ghauri-III[source] | — |
|---|
| Warhead | HE / NE[source] | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] |
|---|
| Blast yield | 12 kilotons of TNT (50 TJ)—35 kilotons of TNT (150 TJ)[source] | — |
|---|
| Engine | Single Stage[source] | Solid-fueled engine[source] |
|---|
| Payload capacity | 760 kg (1,680 lb)–1,158 kg (2,553 lb)[source] | — |
|---|
| Transmission | Manual[source] | — |
|---|
| Suspension | Atego x 8WD semi-trailer (with Pakistani military markings)[source] | — |
|---|
| Propellant | Liquid-propellant Fuel: TM-185 (20% Gasoline 80% Kerosene ) Oxidizer: AK-27I (73% HNO 3 , 27% N 2 O 4 )[source] | Solid composite[source] |
|---|
| Fuel capacity | 12,912 kg (28,466 lb)[source] | — |
|---|
| Flight altitude | 350 km (220 mi) 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] |
|---|
| Accuracy | 190 m (620 ft) CEP[source] | 35–200 m (115–656 ft)[source] |
|---|
| Launch platform | Launch pad[source] | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] |
|---|
| Alternative designation | Ghauri–I[source] | — |
|---|
| Wars | — | Russo-Ukrainian war[source] |
|---|
| Developed into | — | See § Variants[source] |
|---|