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| Name / Designation | Sejjil, Sejil, Sajjil, Ashoura |
| Type / Role | Two-stage Medium-Range Ballistic Missile |
| Country of Origin | Iran |
| Manufacturer | Iranian domestic defense industry |
| Service Entry / Year Introduced | Reported in service from 2012 |
| Operational Status | Operational status reported, although current status is described as uncertain by CSIS |
| Range | Approximately 2,000 km |
| Speed | Not publicly confirmed |
| Ceiling / Altitude Limit | Not reliably disclosed |
| Accuracy (CEP) | Not reliably disclosed |
| Warhead Type | High explosive; assessed nuclear-capable delivery role |
| Guidance System | Inertial navigation; later guidance upgrades reported |
| Targeting Mode | Ballistic trajectory with onboard guidance |
| Launch Platform Compatibility | Road-mobile TEL |
| Seeker Type | No conventional terminal seeker publicly confirmed |
| Length | Approximately 18 m |
| Diameter | Approximately 1.25 m |
| Wingspan | Not publicly disclosed |
| Launch Weight | Approximately 23,600 kg |
| Propulsion | Two-stage solid propellant |
| Warhead Weight | Reported payload varies, approximately 500 to 1,500 kg |
| Explosive Type | High explosive |
| Detonation Mechanism | Not publicly disclosed |
| Payload Options | Conventional; nuclear-capable delivery is assessed, but no confirmed nuclear warhead deployment |
| Operational Range Type | Medium |
| Deployment Platform | Ground |
| Target Types | Reported operational use, with details subject to limited public evidence |
| Combat Proven | Iran |
The Sejjil missile is an Iranian two-stage, solid-propellant medium-range ballistic missile (MRBM) developed as part of Iran’s effort to field more responsive and mobile long-range strike systems. Unlike Iran’s earlier liquid-fueled Shahab family, Sejjil uses solid propellant, which reduces the need for lengthy fueling preparations before launch. The missile is road-mobile and is associated with a transporter-erector-launcher.
Sejjil was domestically designed and built in Iran. Public sources do not identify a single commercial manufacturer, so it is more accurate to describe its producer as Iran’s domestic defense-industrial sector rather than assigning it to a specific company. Development reportedly began in the late 1990s, with the first known flight test taking place in 2008.
The Sejjil has a reported range of approximately 2,000 km, placing it in the MRBM category. Its two-stage solid-fuel propulsion provides a faster launch preparation cycle than liquid-fueled systems. A precise official maximum speed is not publicly established, so a specific Mach figure should not be treated as confirmed. The missile has a reported launch weight of about 23,600 kg, a length of roughly 18 meters, and a diameter of approximately 1.25 meters.
A reliable public unit price for the Sejjil has not been disclosed. Development, production, launcher, support infrastructure, and missile testing costs are also difficult to separate from Iran’s broader ballistic missile program. Therefore, any precise Sejjil price estimate should be treated as speculative.
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