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At a glance
Hwasong-11Alarger figure on 3 of 3
Pralay (missile)larger figure on 0 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Maximum; 2.08 km/s
Single sourceMaximum; Mach 6.1 (
Single sourceMach 6.1 (7,470 km/h; 4,640 mph; 2.08 km/s)[source]
Warhead weight · source measurement 1
Single sourceWarhead weight · source measurement 2
Single source350–700 kg (770–1,540 lb) 500–1,000 kg (1,100–2,200 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Hwasong-11A | Pralay (missile) |
|---|---|---|
| Type | Short-range ballistic missile[source] | Tactical ballistic missile[source] |
| Place of origin | North Korea[source] | India[source] |
| In service | 2019–present[source] | — |
| Used by | North Korea ( Korean People's Army Strategic Force ) Russia[source] | Indian Army Indian Air Force[source] |
| Wars | Russo-Ukrainian war[source] | — |
| Designed | 2018[source] | — |
| Manufacturer | February 11 Plant[source] | Bharat Electronics Bharat Dynamics Limited[source] |
| Developed into | See § Variants[source] | — |
| Warhead | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] | HE PF , PCB , RDPS[source] |
| Engine | Solid-fueled engine[source] | Two stage rocket + MaRV[source] |
| Propellant | Solid composite[source] | Solid[source] |
| Flight altitude | 50–60 km (31–37 mi)[source] | — |
| Guidance system | Inertial navigation system (INS), possible satellite navigation[source] | Mid-course: INS Terminal: MMW DSMAC + Radar Imaging[source] |
| Accuracy | 35–200 m (115–656 ft)[source] | <10 metres (33 ft) CEP[source] |
| Launch platform | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] | 12 x 12 Ashok Leyland HMV TEL[source] |
| Designer | — | Research Centre Imarat[source] |
| Reported operators | — |
|