FORCETALLY
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Measured figures
Configuration
| Specification | Abdali-I | Surya missile |
|---|---|---|
| Type | SRBM[source] | Intercontinental ballistic missile[source] |
| Place of origin | Pakistan[source] | India[source] |
| Used by | Pakistan Army Army Strategic Forces Command[source] | Indian Armed Forces[source] |
| Designer | SUPARCO (Rocket stage) DESTO (Warhead design/assembly)[source] | Defence Research and Development Organisation |
Diameter
Single source0.56 m (22 in)[source]
Maximum; Mach 27 (
Single sourceMach 27 (33,100 km/h)[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.
| Designed | 1993–97[source] | — |
|---|
| Manufacturer | SUPARCO[source] | Bharat Dynamics Limited[source] |
|---|
| Warhead | Single conventional HE / ICM[source] | 3-15 MIRV warheads with yield 750kt or 5 Mt single warhead[source] |
|---|
| Transmission | Automatic[source] | — |
|---|
| Suspension | MAZ-7310 8WD (With Pakistani military markings)[source] | — |
|---|
| Propellant | Solid-propellent[source] | Solid and liquid fuel[source] |
|---|
| Guidance system | Inertial , Terminal[source] | — |
|---|
| Accuracy | 100 m (330 ft)—150 m (490 ft) CEP .[source] | — |
|---|
| Launch platform | Transporter erector launcher (TEL)[source] | TEL , Missile launch facility[source] |
|---|
| Blast yield | — | 750KT to 5MT[source] |
|---|
| Engine | — | Two-stage solid rocket + third stage solid/ liquid rocket[source] |
|---|