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At a glance
Abdali-Ilarger figure on 0 of 3
Shaheen-IIIlarger 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
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.
Configuration
| Specification | Abdali-I | Shaheen-III |
|---|---|---|
| Type | SRBM[source] | MRBM[source] |
| Place of origin | Pakistan[source] | Pakistan[source] |
| Used by | Pakistan Army Army Strategic Forces Command[source] | Pakistan Army ( Army Strategic Forces Command )[source] |
| Designer | SUPARCO (Rocket stage) DESTO (Warhead design/assembly)[source] | National Engineering & Scientific Commission (NESCOM)[source] |
| Designed | 1993–97[source] | 2003–2013[source] |
| Manufacturer | SUPARCO[source] | National Engineering & Scientific Commission[source] |
| Warhead | Single conventional HE / ICM[source] | HE / NE[source] |
| Transmission | Automatic[source] | Automatic[source] |
| Suspension | MAZ-7310 8WD (With Pakistani military markings)[source] | WS21200 16WD (with Pakistani military markings)[source] |
| Propellant | Solid-propellent[source] | Solid-fuel[source] |
| Guidance system | Inertial , Terminal[source] | Inertial , Terminal ,[source] |
| Accuracy | 100 m (330 ft)—150 m (490 ft) CEP .[source] | — |
| Launch platform | Transporter erector launcher (TEL)[source] | Transporter erector launcher (TEL), launch pad[source] |
| In service | — | 2015–present[source] |
| Variants | — | Ababeel[source] |
| Blast yield | — | >50 kilotons of TNT (210 TJ)[source] |
| Engine | — | Multi-stage[source] |