Bayraktar Mini
| Bayraktar Mini UAV | |
|---|---|
 Artist impression | |
| General information | |
| Type | Miniature UAV |
| National origin | Turkey |
| Manufacturer | Baykar |
| Status | Active since December 2007 |
| Primary user | Turkish Armed Forces |
| Number built | 500+ |
| History | |
| Manufactured | 2005 |
| First flight | October 2006 |
The Bayraktar Mini UAV is a miniature UAV produced by the Turkish company Baykar.[1][2]
Development
[edit | edit source]System design activities started in 2004 with the concept of short range day and night aerial reconnaissance and surveillance applications. The initial prototype, Bayraktar A, was developed in 2005, and following successful autonomous flight demonstrations, Baykar received a contract to begin serial production. The first batch of the order by the Turkish Armed Forces was composed of 19 aircraft which were mainly deployed to the southeast parts of Turkey to be used in counterterrorism operations.[3] After hundreds of hours flight trials and feedback, the system was subjected to major modifications and a superior version began development. The Bayraktar B Mini UAV System was completed and became operational in December 2007 to be 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 development of the aircraft is being continued. According to the company, the most recent version, the Bayraktar MINI UAV D, has 2 times greater communication range and 3 times higher maximum altitude compared to its predecessors.[8][9]
Overview
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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]
The main features of the Bayraktar B are:
- Automatic waypoint navigation
- Secure digital communication
- Home return and automatic parachute landing in case of lost communication
- Smart battery management system
- Remote-range command/control and monitor (WAN Relay)
- Ground control switching
- Automatic take off
- Automatic cruising
- Automatic belly landing / parachute deployment
- Joystick assisted semi-automatic control
- Automatic stall control in case of electric motor dysfunction
- Automatic spin control in case of very harsh wind conditions
- Real-time Google Earth integration (display of telemetry data, routes etc. in real-time)
- On-screen video display
- Target coordinate estimation with an accuracy of within 10 meters
- Automatic tracking antenna system
- Enhancing Situational Awareness by FLIR's Tau Core[13]
Operators
[edit | edit source]Confirmed Operators Of Bayraktar Mini UAV
[edit | edit source]
Specifications
[edit | edit source]
| Specification | Bayraktar A | Bayraktar B | Notes | Ref |
|---|---|---|---|---|
| Length | 1.2 m (3 ft 11 in) | 1.2 m (3 ft 11 in) | [15] | |
| Wing Span | 1.6 m (5 ft 3 in) | 1.9 m (6 ft 3 in) | [15] | |
| Weight | 3.5 kg (7.7 lb) | 4.5 kg (9.9 lb) | [15] | |
| Power / Source | Electric / Battery | Electric / Battery | [15] | |
| Take Off | Hand Launch | Hand Launch | [15] | |
| Landing | Over Fuselage | Over Fuselage | [15] | |
| Communication Range | 10 km (6.2 mi)[citation needed] | 15 km (9.3 mi)[15] With Auto Tracking Antenna System[citation needed] | ||
| Endurance | > 60 minutes | > 60 minutes (with 1000 meters operational Altitude) | [16] | |
| Operational Altitude | 1,000 ft (300 m) | 3,000 ft (910 m) | [15] | |
| Maximum Altitude | 12,000 ft (3,700 m) | 12,000 ft (3,700 m) | [citation needed] | |
| Cruise Speed | 70 km/h (43 mph) | 110 km/h (68 mph) | [15] | |
| Payload 1 | CCD Camera (Fixed Mount) | CCD Camera (Tilt Axis Movement) | CCD Camera (2 Axis Movement) | [citation needed] |
| Payload 2 | Thermal Camera (Fixed Mount) | Thermal Camera (Tilt Axis Movement) | Thermal Camera (2 Axis Movement) | [citation needed] |
| Structure | Composite material | Composite material | [15] | |
| Operating Crew | 2 | 2 | [citation needed] |
References
[edit | edit source]- ^ a b Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Turkish army orders mini-UAVs Archived 2013-10-03 at the Wayback Machine, 8 August 2006
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
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- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Turkey's Kalebaykar reveals VTOL UAV demonstrator test programme Archived 2011-08-11 at the Wayback Machine, 14 August 2006
- ^ Bayraktar Mini UAV system brochure Archived July 18, 2014, at the Wayback Machine, Baykar Makina
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
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