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Measured figures
Configuration
| Specification | Ababeel (missile) | Hwasong-11A |
|---|---|---|
| Type | MIRV surface-to-surface missile ballistic missile[source] | Short-range ballistic missile[source] |
| Place of origin | Pakistan[source] | North Korea[source] |
| In service | 2017 –Present[source] | 2019–present[source] |
| Used by | Pakistan Army ( Army Strategic Forces Command )[source] |
Height
Single source21.5 m (71 ft)[source]
Mass
Single source3,415–8,729 kg (7,529–19,244 lb)[source]
3-8 MIRVs 3 Warheads of each (standard) 5 Warheads of
Single sourceeach
Single sourceeach 8 Warheads of
Single source3-8 MIRVs 3 Warheads of 500kg each (standard) 5 Warheads of 300kg each 8 Warheads of 185kg each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
North Korea ( Korean People's Army Strategic Force ) Russia[source]
| Designed | 2010–2017[source] | 2018[source] |
|---|
| Manufacturer | National Engineering & Scientific Commission (NESCOM)[source] | February 11 Plant[source] |
|---|
| Warhead | HE / NE[source] | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] |
|---|
| Blast yield | >50 kilotons of TNT (210 TJ)[source] | — |
|---|
| Transmission | Automatic[source] | — |
|---|
| Suspension | WS21200 16WD (With Pakistani military markings)[source] | — |
|---|
| Propellant | Solid-fuel[source] | Solid composite[source] |
|---|
| Guidance system | Inertial , Terminal[source] | Inertial navigation system (INS), possible satellite navigation[source] |
|---|
| Launch platform | Transporter erector launcher (TEL), Launch pad[source] | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] |
|---|
| Wars | — | Russo-Ukrainian war[source] |
|---|
| Developed into | — | See § Variants[source] |
|---|
| Engine | — | Solid-fueled engine[source] |
|---|
| Flight altitude | — | 50–60 km (31–37 mi)[source] |
|---|
| Accuracy | — | 35–200 m (115–656 ft)[source] |
|---|