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At a glance
DF-31larger figure on 2 of 2
Tondar-69larger figure on 0 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source21.6 m (70 ft 10 in)[source]
Length
Single sourceConfiguration
| Specification | DF-31 | Tondar-69 |
|---|---|---|
| Speed | Up to 8.16 km/s (Mach 25)[source] | — |
| Type | Intercontinental ballistic missile[source] | Short range ballistic missile[source] |
| Place of origin | People's Republic of China[source] | — |
| In service | 2006 (DF-31), 2007 (DF-31A), 2017 (DF-31B)[source] | — |
| Used by | People's Liberation Army Rocket Force[source] | Iran[source] |
10.8 m[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufacturer | Academy of Rocket Motors Technology (ARMT)[source] | Defense Industries Organization[source] |
|---|
| Unit cost | — |
|---|
| Warhead | 425 kilotonnes of TNT (1,780 TJ)[source] | Single warhead[source] |
|---|
| Engine | Solid-fuel rocket[source] | Two-stage : solid -fuel booster and liquid fuel sustainer[source] |
|---|
| Flight altitude | Up to 1,200 km (750 mi)[source] | — |
|---|
| Guidance system | Astro-inertial guidance with BeiDou Navigation Satellite System[source] | Inertial with command updates[source] |
|---|
| Accuracy | 100 m CEP for silo launched and 150–300 m for TEL-launched.[source] | 50 m – 150 m CEP[source] |
|---|
| Launch platform | Silo, 8 axle TEL[source] | — |
|---|
| Country of origin | — | Iran[source] Iran[source] |
|---|