HESA Karrar
Summary
| Category | Military Drones |
| Origin country | 🇮🇷 Iran |
| Manufacturer | HESA |
| First flight | 1 January 2010 |
| Year introduced | 2010 |
Technical specifications
| Version: Standard | |
|---|---|
| Operational range | 1,000 km (621 mi) |
| Maximum speed | 900 km/h (559 mph) |
| Wingspan | 2.5 m (8.2 ft) |
| Length | 4 m (13.1 ft) |
| Max. takeoff weight | 700 kg (1,543 lbs) |
| Powerplant | 1 x Tolloue 5 or Microturbo TRI 60-5 turbojet delivering 4 kN each |
All operators
Armament
Missiles payload:
- Air-to-Air Short-Range Majid
- Air-to-Air Short-Range Shahab-e-Saqeb
- Anti-Ship Kowsar
- Anti-Ship Nasr-1
Bombs payload:
- Guided Bomb Mk 82 PGM
- Guided Bomb Balaban
- Unguided Bomb Mk 81
- Unguided Bomb Mk 82
Description
The HESA Karrar is an Iranian jet-powered unmanned aerial vehicle (UAV) produced by the Iran Aircraft Manufacturing Industrial Company (HESA) since 2010. Developed during the Ahmadinejad presidency, the aircraft is a derivative of the 1970s-era American Beechcraft MQM-107 Streaker, incorporating design elements from the South African Denel Dynamics Skua. Development was underway as of 2002, potentially under the designation "Hadaf-1," with a subscale model appearing in 2004. The aircraft was officially unveiled on August 23, 2010.
The Karrar features a cylindrical, blunt-nosed fuselage with a low-mounted, clipped delta wing and high-mounted twin arrowhead-shaped endplate tailfins. It is powered by a single Tolloue 5 or Microturbo TRI 60-5 turbojet engine producing approximately 4.2–4.4 kN of thrust, fed by a dorsal air intake. The aircraft utilizes a rocket-assist system for launch and is recovered by parachute; Iranian officials also claim air-launch capability. Avionics include an autopilot system with INS and GPS guidance, allowing for pre-programmed flight paths that can be updated in flight. The Karrar is capable of high and low altitude flight during day or night and may possess terrain-following capabilities. The platform lacks visible electro-optical or infrared (EO/IR) sensors.
The aircraft has a maximum takeoff weight of 700 kg and a payload capacity of 227 kg (500 lb) across three hardpoints. The centerline station can carry a single 500 lb Mk 82 general-purpose bomb or a Mark 46 torpedo. Underwing stations carry two Nasr-1 or Kowsar anti-ship missiles, or two 250 lb Mk 81 bombs. Since 2019, the Karrar has been integrated with the Balaban satellite-guided glide bomb. For air-to-air engagements, the platform is equipped with Shahab-e-Saqeb missiles or the Majid heat-seeking missile, which has an 8 km range. Carrying weapons reduces the aircraft's operational range.
The Islamic Republic of Iran Air Defense Force uses the Karrar primarily as a target drone to simulate aerial threats for training air-defense crews. It has been used to test various systems, including Mersad, S-300PMU-2, and Sayyad-2/3 surface-to-air missiles, as well as Fakour-90 air-to-air missiles. Although initially framed as a "long-range bomber drone," the first recorded deployment of munitions by a Karrar occurred during a 2020 exercise. The platform has been exported to Hezbollah and has reportedly been used in the Syrian Civil War. Specifications include a maximum speed of 900 km/h and a maximum range of 1,000 km.