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| Name / Designation | Fateh-110 |
| Type / Role | Short Range Ballistic Missile, Surface to Surface |
| Country of Origin | Iran |
| Manufacturer | Iranian defense industry |
| Service Entry / Year Introduced | Approximately 2004 |
| Operational Status | Operational |
| Range | Approximately 200 to 300 km |
| Speed | Not reliably disclosed |
| Ceiling / Altitude Limit | Not publicly established |
| Accuracy (CEP) | Varies by variant; approximately 250 to 500 m has been reported for related configurations |
| Warhead Type | High explosive; other payloads have been reported in assessments |
| Guidance System | Guidance and flight control system; GPS guidance reported for some configurations |
| Targeting Mode | Preprogrammed precision strike |
| Launch Platform Compatibility | Road mobile ground launcher |
| Seeker Type | No conventional terminal seeker publicly confirmed for the baseline Fateh 110 |
| Length | 8.86 m |
| Diameter | 0.61 m |
| Wingspan | Not reliably disclosed |
| Launch Weight | Approximately 3,450 kg |
| Propulsion | Single stage solid propellant |
| Warhead Weight | Approximately 450 to 600 kg |
| Explosive Type | High explosive; submunition and chemical payloads have been reported in assessments |
| Detonation Mechanism | Not reliably disclosed |
| Payload Options | Conventional payloads; no credible evidence establishes the baseline Fateh 110 as nuclear capable |
| Operational Range Type | Short |
| Deployment Platform | Ground |
| Target Types | Military facilities, fixed installations and other regional targets |
| Combat Proven | Yes |
| Users / Operators | Iran; Fateh family variants have also been associated with regional transfers |
The Fateh-110 is an Iranian, road mobile, short range ballistic missile developed for surface to surface strikes against targets within the surrounding region. Iran began developing the system in the 1990s, with early flight testing reported in 2001. The missile is generally assessed as a development of the unguided Zelzal 2 rocket family, incorporating guidance and flight control systems.
The Fateh-110 Missile uses a single stage solid propellant motor, allowing comparatively rapid launch preparation because the missile does not require liquid fuel loading immediately before launch. It is carried by mobile launch systems, supporting dispersal and relocation after deployment.
The Fateh-110 Missile program is indigenous to Iran, although assessments have identified possible Chinese assistance or components during its development. No single commercial manufacturer is consistently identified in open sources, so it is more accurate to describe it as an Iranian defense industry program. The missile entered Iranian service around 2004 and remains operational.
The standard Fateh-110 is generally assessed to have a range of approximately 200 to 300 km, placing it in the short range ballistic missile category. Its launch weight is about 3,450 kg, while its payload is commonly estimated at roughly 450 to 600 kg.
A precise publicly verified maximum speed is not consistently available, so a Mach figure should not be presented as definitive. Later members of the Fateh family, including the Fateh 313, extend the range to about 500 km.
There is no reliable publicly disclosed unit price for the Fateh-110. Production costs are influenced by missile configuration, launcher equipment, guidance components, and procurement arrangements. Any specific dollar figure should therefore be treated cautiously.
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