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At a glance
9K720 Iskanderlarger figure on 0 of 3
Hwasong-11Alarger 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
Maximum; Maximum speed
Single source2100 m/s[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | 9K720 Iskander | Hwasong-11A |
|---|---|---|
| Type | Short-range ballistic missile[source] | Short-range ballistic missile[source] |
| Place of origin | Russia[source] | North Korea[source] |
| In service | 2006–present[source] | 2019–present[source] |
| Used by | Russian Ground Forces Armenian Armed Forces Algerian People's National Army Armed Forces of Belarus[source] | North Korea ( Korean People's Army Strategic Force ) Russia[source] |
| Wars | Russo-Georgian War Syrian Civil War Second Nagorno-Karabakh War Russo-Ukrainian war[source] | Russo-Ukrainian war[source] |
| Designed | From 1988[source] | 2018[source] |
| Manufacturer | Missiles: Votkinsk Plant State Production Association ( Votkinsk ) Ground equipment: Production Association Barricades ( Volgograd ) System developer: KBM ( Kolomna )[source] | February 11 Plant[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] | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] |
| Engine | Single-stage solid propellant[source] | Solid-fueled engine[source] |
| Guidance system | Iskander-M : INS + GLONASS + DSMAC Iskander-K : INS + GLONASS + TERCOM[source] | Inertial navigation system (INS), possible satellite navigation[source] |
| Launch platform | Mobile transporter erector launcher[source] | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] |
| 9P78 | P78 launcher: 2[source] | — |
| 9T250 | 250 transloader: 2[source] | — |
| Developed into | — | See § Variants[source] |
| Propellant | — | Solid composite[source] |
| Flight altitude | — | 50–60 km (31–37 mi)[source] |
| Accuracy | — | 35–200 m (115–656 ft)[source] |
| Reported operators |
| — |