FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Hatf-Ilarger 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
Length
Single source6.0 m (19.7 ft)[source]
Length
Single sourceConfiguration
| Specification | Hatf-I | Hwasong-11A |
|---|---|---|
| Type | Short-range ballistic missile[source] | Short-range ballistic missile[source] |
| Place of origin | Pakistan[source] | North Korea[source] |
| In service | 1992 –Present[source] | 2019–present[source] |
| Used by | Pakistan Army Air Defense Corps (1992–99) Air Defense Command (1999-2000) Army Strategic Forces Command (2000–Present)[source] | North Korea ( Korean People's Army Strategic Force ) Russia |
8.77 m (28.8 ft)[source]
Maximum; Maximum speed
Single source5.9–6.1 m/s (19–20 ft/s)[source]
Warhead weight
Single source500 kg (1,100 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Space Research Commission (Rocket system) Kahuta Research Laboratories (Warhead design/assembly)[source] | — |
|---|
| Designed | 1987–89[source] | 2018[source] |
|---|
| Manufacturer | Space Research Commission[source] | February 11 Plant[source] |
|---|
| Produced | 1987–2001[source] | — |
|---|
| No. built | 105 (stock estimated in 2021) )[source] | — |
|---|
| Variants | Hatf-I: 1992 Hatf-IA: 1995 Hatf-IB: 2001[source] | — |
|---|
| Warhead | Conventional HE / CE[source] | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] |
|---|
| Engine | Single-stage[source] | Solid-fueled engine[source] |
|---|
| Payload capacity | 500 kg (1,100 lb)[source] | — |
|---|
| Transmission | Manual[source] | — |
|---|
| Suspension | M35 / Isuzu x 4WD semi-trailer[source] | — |
|---|
| Propellant | Solid-propellant[source] | Solid composite[source] |
|---|
| Guidance system | Unguided :Hatf-I/IA Inertial : Hatf-IB[source] | Inertial navigation system (INS), possible satellite navigation[source] |
|---|
| Accuracy | 100 m (330 ft) CEP[source] | 35–200 m (115–656 ft)[source] |
|---|
| Launch platform | Transporter erector launcher[source] | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] |
|---|
| Wars | — | Russo-Ukrainian war[source] |
|---|
| Developed into | — | See § Variants[source] |
|---|
| Flight altitude | — | 50–60 km (31–37 mi)[source] |
|---|