FORCETALLY
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Measured figures
Maximum; Mach 27 (
Single sourceMach 27 (33,100 km/h)[source]
Shaheen-I
Single sourceShaheen-IA
Single source700 kg (1,500 lb) (Shaheen-I) 1,000 kg (2,200 lb) (Shaheen-IA)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Shaheen-I | Surya missile |
|---|---|---|
| Type | SRBM[source] | Intercontinental ballistic missile[source] |
| Place of origin | Pakistan[source] | India[source] |
| In service | 2003 –Present[source] | — |
| Used by | Pakistan Army ( Army Strategic Forces Command )[source] | Indian Armed Forces[source] |
| Designer | National Defence Complex[source] | Defence Research and Development Organisation[source] |
| Designed | 1995–99[source] | — |
| Manufacturer | National Defence Complex National Engineering & Scientific Commission[source] | Bharat Dynamics Limited[source] |
| Variants | Shaheen-I: 700Km Shaheen-IA: 1000Km[source] | — |
| Warhead | HE / ICM / NE[source] | 3-15 MIRV warheads with yield 750kt or 5 Mt single warhead[source] |
| Blast yield | 35 kilotons of TNT (150 TJ) (Shaheen-I) 40 kilotons of TNT (170 TJ) (Shaheen-IA)[source] | 750KT to 5MT[source] |
| Engine | Single-stage[source] | Two-stage solid rocket + third stage solid/ liquid rocket[source] |
| Transmission | Automatic[source] | — |
| Suspension | MAZ-7310 8WD (With Pakistani military markings)[source] | — |
| Propellant | Solid-propellant[source] | Solid and liquid fuel[source] |
| Guidance system | Inertial , Terminal[source] | — |
| Accuracy | <50 m (160 ft) CEP[source] | — |
| Launch platform | Transporter erector launcher (TEL), launch pad[source] | TEL , Missile launch facility[source] |