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At a glance
9K720 Iskanderlarger figure on 0 of 3
DF-31larger figure on 3 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source7.3 m (24 ft)[source]
Length
Single sourceConfiguration
| Specification | 9K720 Iskander | DF-31 |
|---|---|---|
| Type | Short-range ballistic missile[source] | Intercontinental ballistic missile[source] |
| Place of origin | Russia[source] | People's Republic of China[source] |
| In service | 2006–present[source] | 2006 (DF-31), 2007 (DF-31A), 2017 (DF-31B)[source] |
| Used by | Russian Ground Forces Armenian Armed Forces Algerian People's National Army Armed Forces of Belarus[source] | People's Liberation Army Rocket Force |
21.6 m (70 ft 10 in)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Russo-Georgian War Syrian Civil War Second Nagorno-Karabakh War Russo-Ukrainian war[source] | — |
|---|
| Designed | From 1988[source] | — |
|---|
| Manufacturer | Missiles: Votkinsk Plant State Production Association ( Votkinsk ) Ground equipment: Production Association Barricades ( Volgograd ) System developer: KBM ( Kolomna )[source] | Academy of Rocket Motors Technology (ARMT)[source] |
|---|
| Unit cost | US$3 million (missile)[source] |
|---|
| Warhead | 480–700 kg (1,060–1,540 lb) thermonuclear weapon , high-explosive fragmentation, submunition , penetration, fuel–air explosive , EMP[source] | 425 kilotonnes of TNT (1,780 TJ)[source] |
|---|
| Engine | Single-stage solid propellant[source] | Solid-fuel rocket[source] |
|---|
| Guidance system | Iskander-M : INS + GLONASS + DSMAC Iskander-K : INS + GLONASS + TERCOM[source] | Astro-inertial guidance with BeiDou Navigation Satellite System[source] |
|---|
| Launch platform | Mobile transporter erector launcher[source] | Silo, 8 axle TEL[source] |
|---|
| 9P78 | P78 launcher: 2[source] | — |
|---|
| 9T250 | 250 transloader: 2[source] | — |
|---|
| Flight altitude | — | Up to 1,200 km (750 mi)[source] |
|---|
| Accuracy | — | 100 m CEP for silo launched and 150–300 m for TEL-launched.[source] |
|---|
| Reported operators |
| — |
|---|