FORCETALLY
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Measured figures
Configuration
| Specification | Shaheen-II | Surya missile |
|---|---|---|
| Type | MRBM[source] | Intercontinental ballistic missile[source] |
| Place of origin | Pakistan[source] | India[source] |
| In service | 2014 –Present[source] | — |
| Used by | Pakistan Army Army Strategic Forces Command[source] | Indian Armed Forces[source] |
Diameter
Single source1.4 m (55 in)[source]
Maximum; Mach 27 (
Single sourceMach 27 (33,100 km/h)[source]
Warhead weight
Single source1,230 kg (2,710 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | National Engineering & Scientific Commission[source] | Defence Research and Development Organisation[source] |
|---|
| Designed | 2000–2013[source] | — |
|---|
| Manufacturer | National Engineering & Scientific Commission[source] | Bharat Dynamics Limited[source] |
|---|
| Warhead | HE / NE[source] | 3-15 MIRV warheads with yield 750kt or 5 Mt single warhead[source] |
|---|
| Blast yield | >40 kilotons of TNT (170 TJ)[source] | 750KT to 5MT[source] |
|---|
| Engine | Two-stage[source] | Two-stage solid rocket + third stage solid/ liquid rocket[source] |
|---|
| Transmission | Automatic[source] | — |
|---|
| Suspension | MAZ-547A 12WD (With Pakistani military markings)[source] | — |
|---|
| Propellant | Solid-propellant[source] | Solid and liquid fuel[source] |
|---|
| Guidance system | Inertial , Terminal[source] | — |
|---|
| Accuracy | <350 m (1,150 ft) CEP[source] | — |
|---|
| Launch platform | Transporter erector launcher (TEL), launch pad[source] | TEL , Missile launch facility[source] |
|---|