Bayraktar Mini UAV is a miniature UAV produced by Turkish company Baykar.[1][2]
Bayraktar Mini UAV | |
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Artist impression | |
Role | Miniature UAV Type of aircraft |
National origin | Turkey |
Manufacturer | Baykar |
First flight | October 2006 |
Status | Active Since December 2007 |
Primary user | Turkish Armed Forces |
Produced | 2005 |
Number built | 500+ |
With the concept of short range day and night aerial reconnaissance and surveillance applications, system design activities started within 2004. Initial prototype Bayraktar A has been developed in 2005, and following successful autonomous flight demonstrations, Baykar has been awarded with a contract to start serial production. The first batch of the order by the Turkish Armed Forces was composed of 19 aircraft and they were mainly deployed to the Southeast parts of Turkey to be used in counterterrorism operations.[3] After hundreds of hours flight trials and feed backs, system was subjected to major modifications and superior versions were started to developed. As a result, Bayraktar B Mini UAV Systems fielded and became operational in December 2007 to be initially operated by the Turkish Armed Forces.[4][5] Due to its success in the region, the system was also awarded with an export deal to the Qatar Armed Forces in 2012.[6][7] The developments over the aircraft is being continued. According to the company the most recent version Bayraktar MINI UAV D version has 2 times greater communication range and 3 times higher maximum altitude comparing to its predecessors.[8] [9]
Bayraktar-B is a hand-launched, portable UAV system, designed to operate under harsh geographic and meteorological conditions.[10][11] Bayraktar-B is fielded with small army units, and as of 2021 have recorded more than 100,000 flight hours.[12] System offers a complete autonomy with protective features with a high rank of reliability and easiness for the operators, which makes it a valuable technological asset.[citation needed]
Main features are:
Bayraktar Mini UAS is operational since 2007.[14]
![]() | This section does not cite any sources. (January 2021) |
Specification | Bayraktar A | Bayraktar B | Notes |
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Length | 1.2 m (3 ft 11 in) | 1.2 m (3 ft 11 in) | |
Wing Span | 1.6 m (5 ft 3 in) | 1.9 m (6 ft 3 in), optional 2.5 m (8 ft 2 in) | |
Weight | 3.5 kg (7.7 lb) | 4.5 kg (9.9 lb) | |
Power / Source | Electric / Battery | Electric / Battery | |
Take Off | Hand Launch | Hand Launch | |
Landing | Belly Landing | Belly Landing / Parachute Landing | |
Communication Range | 10 km (6.2 mi) | 15 km (9.3 mi) With Auto Tracking Antenna System | |
Endurance | > 60 minutes | > 60 minutes (with 1000 meters operational Altitude) | |
Operational Altitude | 1,000 ft (300 m) | 3,000 ft (910 m) | |
Maximum Altitude | 12,000 ft (3,700 m) | 12,000 ft (3,700 m) | |
Cruise Speed | 70 km/h (43 mph) | 55 km/h (34 mph) | |
Payload 1 | CCD Camera (Fixed Mount) | CCD Camera (Tilt Axis Movement) | CCD Camera (2 Axis Movement) |
Payload 2 | Thermal Camera (Fixed Mount) | Thermal Camera (Tilt Axis Movement) | Thermal Camera (2 Axis Movement) |
Structure | Composite material | Composite material | |
Operating Crew | 2 | 2 |