| Ababil-100/Al Fat'h | |
|---|---|
 An al-Fat'h missile | |
| Type | Short-range ballistic missile |
| Place of origin | Iraq[1] |
| Service history | |
| In service | 2003 |
| Wars | Iraq War |
| Production history | |
| Variants | Guided version Unguided version |
| Specifications | |
| Mass | 1200 kg |
| Length | 6.7 m |
| Diameter | 0.5 m 1.4 m aft fin assembly |
| Payload capacity | 260-300 kg HE Guided version:HE Unguided version:HE and submunition |
| Propellant | 828 kgsolid propellant Composition: 70% AP 14% Aluminium powder 11-12% HTPB 3.5% DIO 1% Ferric Oxide 1% TDI 0.35% MAPO[citation needed] |
Operational range | >150 km |
Guidance system | Unguided version:Fin stabilized Guided version:Inertial guidance |
| References | |
The Ababil-100 or al-Fat'h or al-Fatah was an Iraqi single stage solid-propelled short-range ballistic missile whose development started around 1991 and was tested from 2000 to 2002. Its launcher was derived from the Ababil-50 MLRS.[2]
- ^ "Ababil-100/Al-Samoud". Federation of American Scientists. Archived from the original on 15 April 2019.
- ^ Altobchi, Cooper & Fontanellaz 2022, p. 57