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At a glance
DF-31larger figure on 3 of 3
Ghauri (missile)larger figure on 0 of 3
Measured figures
Length
Single source21.6 m (70 ft 10 in)[source]
Length
Single sourceConfiguration
| Specification | DF-31 | Ghauri (missile) |
|---|---|---|
| Speed | Up to 8.16 km/s (Mach 25)[source] | — |
| Type | Intercontinental ballistic missile[source] | MRBM[source] |
| Place of origin | People's Republic of China[source] | Pakistan[source] |
| In service | 2006 (DF-31), 2007 (DF-31A), 2017 (DF-31B)[source] | 2003 –present[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
15.90 m (52.2 ft)[source]
Operational; DF-31
Single sourceOperational; DF-31A
Single source7,200–8,000 km (4,500–5,000 mi) (DF-31) 13,200 km (8,200 mi) (DF-31A)[source]
Maximum; Maximum firing range
Single sourceOperational; Operational range
Single sourceWarhead 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.
| Used by |
|---|
People's Liberation Army Rocket Force[source] |
Pakistan Army ( Army Strategic Forces Command )[source] |
| Manufacturer | Academy of Rocket Motors Technology (ARMT)[source] | Khan Research Laboratories[source] |
|---|
| Unit cost | — |
|---|
| Warhead | 425 kilotonnes of TNT (1,780 TJ)[source] | HE / NE[source] |
|---|
| Engine | Solid-fuel rocket[source] | Single Stage[source] |
|---|
| Flight altitude | Up to 1,200 km (750 mi)[source] | 350 km (220 mi) reached in first test flight[source] |
|---|
| Guidance system | Astro-inertial guidance with BeiDou Navigation Satellite System[source] | Inertial , Terminal[source] |
|---|
| Accuracy | 100 m CEP for silo launched and 150–300 m for TEL-launched.[source] | 190 m (620 ft) CEP[source] |
|---|
| Launch platform | Silo, 8 axle TEL[source] | Launch pad[source] |
|---|
| Designer | — | Khan Research Laboratories (KRL)[source] |
|---|
| Designed | — | 1994–2001[source] |
|---|
| No. built | — | 30 (estimated 2021)[source] |
|---|
| Variants | — | Ghauri-II , Ghauri-III[source] |
|---|
| Blast yield | — | 12 kilotons of TNT (50 TJ)—35 kilotons of TNT (150 TJ)[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] |
|---|
| Fuel capacity | — | 12,912 kg (28,466 lb)[source] |
|---|
| Alternative designation | — | Ghauri–I[source] |
|---|