UAV Solutions

Unmanned Aerial Vwhicle Brochures 

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Aerogard is a UAV design, production and consultancy brand of BMS Defence that its central office is in Ankara. It provides services for Defense, Aviation, Health and Production Industries.

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TOYGAR

Fixed Wing S2000-E

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BOZKUŞ

VTOL V2500-E

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GÖKTUĞ

VTOL V3400-H

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AYBARS

Fixed Wing S4200-H

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BORAN

AEROGARD ATTACK X8

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KORGAN-5

Cargo Drone (5 Kg)

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KORGAN-10

Cargo Hybrid Drone

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GEZGİN

AEROGARD QUAD X4

Tablet Ground Station

Intel Core i7 Processor
10.1” Touch Screen
128 Gb SSD Memory
8 Gb Ram - Windows 10 OS
Radiolink & Datalink (Optional)
Flight and Auto Object Tracking
Video Recording, Target Detection on Map
IP65 / MIL-STD-810G Drop Specifiations

Ground
Station

Radiolink, Datalink & Videolink
1080P Digital HD Video Transmission
Receiver HDMI Input / Ethernet Camera
7” Touch Screen with High Brightness
2 Gb Ram, 16 Gb Rom
5 / 15 Km Range
Android 9.0 OS

5.5’’ Screen Tablet

Radiolink & Telemetry
1080P Digital HD Video Transmission
Receiver HDMI Input / Ethernet Camera
5.5” Touch Screen with High Brightness
2 Gb Ram, 16 Gb Rom, 8-Core CPU
5 / 15 Km Range
Android 9.0 OS

Rugged Ground Station

Intel Core i5 Processor
15.6” Touch Screen
Rugged, Hardcase Bag Design
120 Gb SSD Memory, 8 Gb Ram
Windows 10 OS
Radiolink & Datalink (Optional)
Flight and Auto Object Tracking
Video Recording, Target Detection on Map, Target GPS Coordinate

Thermal Camera

25/50 mm Lens
640 Pix.

Optical Zoom Camera

30x Optical Zoom Camera

Mapping Camera

24mp-36mp-42mp

Optical Zoom Camera

36x Optical Zoom Camera

Dual Sensor Camera

30x Zoom & 640 Px Thermal

Zoom Camera

Laser distance meter 1000m
30x Zoom Camera

Thermal Camera

Dual Sensor Camera
10x Zoom & 320 Px
Thermal Camera

AC-AC Power Unit

Capacity : 4 kVA (4000 W)
Weight : 64.1 kg
Support Period : 10 minutes flight time when mains and generator are off

AC-DC Power Unit

Input Voltage : 220 VAC
Cable Length : 110 m
Cable Weight : 2 kg
Automatic Adjustable Tension Pulley System

Rotary Wing Multirotor UAV

  • Weight : 11600 gr
  • Cable Weight : 2000 gr
  • Dimensions : 113x113x48 cm
  • Body Type and Shape : Hexa X
  • Body Material : Carbon fiber
  • Mission Altitude : 80-90 m
  • Maximum Mission Altitude : 100 m
  • Operating Temperature : -10 ° C / 55 ° C
  • Wind Resistance Speed : 35-40 km/h
  • Operating Time : 4-6 Hours (With Standart Single Aerial Platform)
  • 24 Hours (With Duo Aerial Platform)
  • Maximum Operating Time : 8-10 Hours (With Standart Single Aerial Platform)
  • GNSS : GPS, Glonass, Beidou
  • Motor  : 6001 170 KV (12S)
  • Electronic Speed Controller : 60 a HV
  • Propeller : 20×6 inç (Carbon fiber)
  • Flight Controller : Open source, Originally developed
  • Power and Data Transfer System : Via special cable(Data and Power via Fiber cable)
  • Safety Battery : 2x 6S 6000 mah Li-Po Batarya
  • Battery Flight Time : 5-8 Minutes

Rotary Wing Multirotor UAV

  • Autonomous Flight
  • 8 kg Maximum Take-Off
  • Ground Control Station or Tablet
  • Target Tracking (Optional)
  • Target Coordinate Detection (Optional)
  • Face Recognition – Scanning (Optional)
  • Laser Distance Meter (Optional)
  • Gas Leak Detection (With Camera) (Optional)
  • Body Type : Quadcopter
  • Body Length (Engine to Engine) : 67x67x48 cm
  • Maximum Take Off : 8 kg
  • Autonomous Flight Controller : Pixhawk 2.1 cube open source
  • Cruise Speed : 40 km/h
  • Control Radius : 5 km
  • Flight Time : 40 min
  • Propellers : 24 Inch
  • Working Temperature : -15°C / +50°C
  • Ground Station : i7 processor Windows computer joystick for
    RC, telemetry and data transmission
  • Ground Control Station : Android or Standard RC
  • Flight Controller : GUI (BMS Gözcü) developed by our
    engineers by using current open source codes

Rotary Wing Unmanned Aerial Vehicle

  • Autonomous Flight
  • Dynamic Design Suitable For Load Bearing
  • 5 kg Payload Capacity
  • 24 kg Maximum Take-Off Weight
  • Ground Control Station or Tablet
  • Face Recognition – Scanning (Optional)
  • Laser Distance Meter (Optional)
  • Gas Leak Detection (With Camera) (Optional)
  • Body Type : Octocopter
  • Maximum Take Off Weight : 24 kg
  • Altitude : 1000 Ft.
  • AutonomousFlight Controller : Pixhawk 2.1 cube open source
  • Cruise Speed : 36 km/h
  • Control Radius : 10 km
  • Flight Time : 30 min
  • Propellers : 28 Inch
  • Working Temperature : -10°C / +45°C
  • Ground Station : i7 processor Windows computer joystick for RC,
    telemetry and data transmission
  • Flight Controller : A GUI (BMS Gözcü) developed by our engineers
    by using available open source codes

Tethered UAV

  • Altitude: 100 m
  • Flight Time: 4-6 hours
  • Max. Take Off: 14 kg
  • Max. Viewing Distance with 30x Zoom Camera: 5 km
  • 25 or 50 mm lens 640 x 480 Pixel
    Thermal Camera
  • Autonomous and Manual Flight
    in a Jammer Environment
  • Weight : 11600 gr.
  • Cable Weight : 2000 gr.
  • Dimensions : 113x113x48 cm
  • Body Type and Class : Hexacopter
  • Body Material : Carbon fiber
  • Mission Altitude : 100 m
  • Working Temperature : -10 ° C ~ 50 ° C
  • Wind Resistance Speed : 35-40 km/h
  • GNSS : GPS, Glonass, Beidou, Galileo
  • Propeller : 20×6 inch (Carbonfiber)
  • Flight Controller : Open Source, Unique Development
  • Power and Data Transfer System : Via Special Cable (Over Cable Data and Power)
  • Security Battery : 2x 6S 6000 mAh Li-Po Battery
  • Flight Time With Security Battery : 5-8 min.
  • Max Working Time : 8-10 Hours (With Standard Single Air Platform)
  • Working Time : 4-6 Hours (With Standard Single Air Platform)
    24 Hours (With Double Air Platform)

Electrical Fixed Wing UAV

  • Autonomous Flight Feature
  • Composite Material
  • Streamlined Design
  • Launching from Ramp or Manually
  • Ground Control Station or Industrial Tablet
  • Target Detection – Tracking (Optional)
  • Target Coordinate Detection (Optional)
  • Military, Engineering, Search and Rescue, Surveillance, Discovery
  • Wingspan : 2 m
  • Length : 1,6 m
  • Maximum Take-Off Weight : 8 kg
  • Payload : 850 Gr.
  • Material : Composite
  • Propulsion System : Brushless Motor (Electrical Engine)
  • Range / Data Link : 10 – 25 km
  • Flight Time : 90 – 120 Hours
  • Operational Speed : 50 – 60 km/h
  • Maximum Speed : 90 km/h
  • Flight Altitude : MSL 8.000 ft.

Electrical Fixed Wing UAV

  • Composite Material Streamlined Design
  • Autonomous Flight Feature
  • 1,2 kg Payload Capacity
  • 15” Screen Radio Controller
  • i5 Processor Ground Station (Optional) 10” Screen
  • i7 Industrial Tablet Ground Station (Optional)
  • Target Detection Tracking (Optional)
  • Target Coordinate Detection (Optional)
  • Face Recognition (Optional)
  • Android / Windows Remote Controller (Optional)
  • Discovery, Surveillance and Detection Search and
    Rescue and Damage Assestment Mapping
  • Engineering and Environmental Pollution Detection
  • Wingspan : 2,5 m
  • Body Length : 1,4 m
  • Max. Take Off Weight : 10 kg
  • Standart Take Off Weight : 8 kg
  • Payload : 1,2 kg
  • Cruise Speed : 75 km/h
  • Flight Time : 70 min (Loaded) / 90 min
  • Range / Data Link : 5 – 100 km
  • Control Radius : 10 km
  • Altitude : MSL 10.000 Ft.
  • Positioning Accuracy : 1 cm ± 1 ppm (Optional)
  • Positioning System : GNSS / PPK
  • WRTK / PPK Update Frequency : 20 Hz (Optional)
  • Working Efficiency : 550 Hectare/h
  • Max. Wind Resistance : Level 6 (13 m/s)
  • Working Temparature : -15°C / +50°C
  • IP Level : IP44
  • UAV Assembly Time : 5 min (With 2 person)
  • Carrier Bag : Hardcase / Softcase
  • Aluminum / Composite Metarial

  • Aerodynamic Design

  • Autonomous Flight Feature

  • Ground Control Station or Industrial Tablet

  • Target Detection – Tracking (Optional)

  • Target Coordinate Detection (Optional)

  • Laser Pointer (Optional)

  • Military, Engineering, Search and Rescue, Discovery

  • UAV Type : Fixed Wing

  • Wing Span : 6.0 m

    Body Length : 3,5 m

  • Maximum Take off Weight : 60 kg

  • EFI Engine : 120 cc

  • Payload : 10 kg

  • Material : Composite

  • Range / Data Link : 25 – 200 km

  • Flight Time : 10 Hours

  • Operational Speed : 70 – 80 km/h

  • Maximum Speed : 110 km/h

  • Altitude : MSL 10.000 Ft.

Fixed Wing / VTOL Hybrid UAV

  • Autonomous Flight Feature
  • Composite Material
  • Streamlined Design
  • Runway or Vertical Take-Off and Landing
  • Ground Control Station or Industrial Tablet
  • Target Detection – Tracking (Optional)
  • Target Coordinate Detection (Optional)
  • Face Recognition (Optional)
  • Military, Engineering, Surveillance,
    Search and Rescue

Fixed Wing Hybrid UAV (S3200H)

  • Wingspan : 3,2 m
  • Body Length : 1,8 m
  • Maximum Take-Off Weight : 18 kg
  • Payload : 5 Kg / 1.5 Kg
  • Material : Composite
  • Propulsion System: Internal Combustion EFI Engine Alternator (Optional) 
  • Range / Data Link : 25-100 km
  • Flight Time : 6 Hours
  • Operational Speed: 60 – 70 km/h
  • Maximum Speed : 110 km/h
  • Flight Altitude : MSL 10.000 ft.

VTOL Hybrid UAV (V3400-H)

  • Wingspan : 3,4 m
  • Body Length : 1,8 m
  • Maximum Take-Off Weight : 22 kg
  • Payload : 1,5 kg
  • Material : Composite
  • Propulsion System : Internal Combustion
    EFI Engine Alternator
    (Optional)
  • Range / Data Link : 25-100 km
  • Flight Time : 3 hours
  • Operational Speed : 60 – 70 km/h
  • Maximum Speed : 110 km/h
  • Flight Altitude : MSL 10.000 ft.

Fixed Wing / VTOL Hybrid UAV

  • Autonomous Flight Feature
  • Composite Material
  • Streamlined Design
  • Runway or Vertical Take Off Landing
  • Ground Control Station or Industrial Tablet
  • Target Detection – Tracking (Optional)
  • Target Coordinate Detection (Optional)
  • Face Recognition (Optional)
  • Laser Pointer (Optional)
  • Military, Engineering, Surveillance, Search and Rescue

Fixed Wing Hybrid UAV (S4200-H)

  • Wing Span : 4,2 m
  • Body Length : 2,5 m
  • Maximum Take Off Weight : 50 / 63 kg
  • Payload : 6 kg
  • Propulsion System: Internal Combustion EFI Engine
    Alternator (Optional)
  • Material : Composite
  • Range / Data Link : 25 – 200 km
  • Flight Time : 9 – 10 Hours 
  • Operational Speed : 70 – 80 km/h
  • Maximum Speed : 110 km/h
  • Altitude : MSL 10.000 Ft.

VTOL Hybrid UAV (V4400-H)

  • Wing Span : 4,4 m
  • Body Length : 2,5 m
  • Maximum Take Off Weight : 43 kg
  • Payload : 4 kg
  • Propulsion System: Internal Combustion EFI Engine
    Alternator (Optional)
  • Material : Composite
  • Range / Data Link : 25 – 200 km
  • Flight Time : 5 – 6 Hours
  • Operational Speed : 70 – 80 km/h
  • Maximum Speed : 110 km/h
  • Altitude : MSL 10.000 Ft.

Unmanned Aerial Vwhicle Brochures  (Download PDF)

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