FORCETALLY
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Measured figures
Configuration
| Specification | Qassem Bassir | Surya missile |
|---|---|---|
| Type | Medium-range ballistic missile[source] | Intercontinental ballistic missile[source] |
| Place of origin | Iran[source] | India[source] |
| Used by | Iran[source] | Indian Armed Forces[source] |
| Designer | Islamic Revolutionary Guard Corps Aerospace Force[source] | Defence Research and Development Organisation |
Maximum; Mach 27 (
Single sourceMach 27 (33,100 km/h)[source]
Operational; ~
Single source~12,000-18,000 km[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufacturer | Ministry of Defence and Armed Forces Logistics (Iran)[source] | Bharat Dynamics Limited[source] |
|---|
| Produced | 2025[source] | — |
|---|
| Propellant | Two-stage solid fuel[source] | Solid and liquid fuel[source] |
|---|
| Guidance system | Inertial navigation + electro-optical/infrared terminal seeker[source] | — |
|---|
| Launch platform | Road-mobile TEL[source] | TEL , Missile launch facility[source] |
|---|
| Warhead | — | 3-15 MIRV warheads with yield 750kt or 5 Mt single warhead[source] |
|---|
| Blast yield | — | 750KT to 5MT[source] |
|---|
| Engine | — | Two-stage solid rocket + third stage solid/ liquid rocket[source] |
|---|