Taimoor

The Taimoor is an conventional non-nuclear derivative of the Ra'ad-II ALCM with improved sub-systems. The export variant's range is reportedly capped by engineers to 290 km in order to comply with MTCR policies. Meanwhile, the Pakistan Air Force (PAF) confirmed that the Taimoor had a maximum range of 600 km after announcing a successful test flight of the missile. == Design ==

The Taimoor features a box-shaped fuselage X-type tail control surfaces, mid-body foldable wings, and underside air-intake for a miniature turbojet engine. Furthermore, it also utilizes low-observability design characteristics in its airframe which are aimed at reducing its radar cross-section. Similar to its ancestors of the Ra'ad ALCM series, the Taimoor retains its terrain hugging capability which coupled with its stealthy design makes it an effective weapon for SEAD operations in warfare. According to the PAF, the missile has a range of . The Taimoor weighs less than 1,200 kg, and is capable of cruise flight at an altitude of between 152 m (500 ft) and 6,096 m (20,000 ft) at a subsonic speed and possesses terrain-hugging and sea-skimming capabilities. It also has a launch altitude of between and . == Operational history ==

On 3 January 2026, the first successful test flight of the Taimoor was carried out by the Pakistan Air Force (PAF), in which the missile was launched from a PAF Dassault Mirage III and struck a land target. Later on 21 April 2026, the Pakistan Navy test fired one in anti-ship configuration during which it successfully hit it's target. == Operators ==