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BBallistic missiles
Measured figures
Configuration
| Specification | Qassem Bassir | Rampage (missile) |
|---|---|---|
| Type | Medium-range ballistic missile[source] | — |
| Place of origin | Iran[source] | Israel[source] |
| Used by | Iran[source] | Israeli Air Force Indian Air Force Indian Navy[source] |
| Designer | Islamic Revolutionary Guard Corps Aerospace Force[source] | Elbit Systems , Israel Aerospace Industries[source] |
Diameter
Single source306 mm (1.004 ft)[source]
Maximum; Mach 1.0 – Mach 1.6
Single source350–550 m/s (Mach 1.0 – Mach 1.6)[source]
Operational; Operational range
Single source150–250 km (93–155 mi)[source]
Warhead weight
Single source150 kg (330 lb)[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] | תעש מערכות ו אלביט מערכות מפעל מלמ של התעשייה האווירית[source]Named manufacturer organization |
|---|
| Produced | 2025[source] | — |
|---|
| Propellant | Two-stage solid fuel[source] | Solid fuel[source] |
|---|
| Guidance system | Inertial navigation + electro-optical/infrared terminal seeker[source] | INS + Altimeter + GPS + Two-way Datalink[source] |
|---|
| Launch platform | Road-mobile TEL[source] | F-16 , F-15 , F/A-18E/F , Eurofighter Typhoon , IAI Kfir , Sukhoi Su-30MKI , SEPECAT Jaguar , MiG-29K[source] |
|---|
| Warhead | — | Multi- EFP[source] |
|---|
| Detonation mechanism | — | Radio proximity fuze , Blast fragmentation[source] |
|---|
| Engine | — | Solid-propellant rocket[source] |
|---|
| Flight altitude | — | 3,000–40,000 ft (910–12,190 m)[source] |
|---|
| Accuracy | — | 10m CEP[source] |
|---|