Product case
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Product case
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Product case presentation
DF3 (loitering munitions, comparable to the Switchblade 300)
Wingspan: 800~920mm (wings can be truncated)
Length: 650~900mm (fuselage head can be replaced)
Power Unit: Motor
Maximum take-off weight: 3~4kg
Maximum load weight: 300g~500g
Cruising speed: 26~30m/s
Maximum speed: >40m/s
Maximum endurance: >20min
Ceiling: >4000m
Take-off and landing mode: barrel launch
Operation: autonomous route, one-click return
Material: carbon fiber structure, modular design, easy maintenance
The FY-180 is an unmanned aerial vehicle (UAV) with a delta wing layout. Its nose is oblate in shape and it adopts a wing-body fusion design, which reduces drag and increases efficiency, and features a compact structure. With the design of large fuel tanks integrated into both the wings and the fuselage, its endurance can reach up to 2,000 kilometers. It has a pusher-type power arrangement, and the propeller has high efficiency. It is a high-performance and low-cost loitering munition.
It uses the catapult takeoff method and can be launched through a launcher or from a vehicle-mounted system, making it convenient for combat deployment. It already has the capability of mass production.
As a smart loitering munition that can be used for a variety of combat missions, the FY-70 combines the characteristics of an unmanned aerial vehicle (UAV) and a guided bomb. It can not only loiter in the mission airspace for a long time and perform various tasks like a UAV, but also quickly approach and precisely strike enemy targets just like a guided bomb or even a missile. The FY-70 model already has the capability of mass production.
Parameters:
• Maximum takeoff weight: 130Kg
• Maximum flight speed: 20m/s
• Cruise speed: 15m/s
• Maximum flight altitude: 3000m
• Wheelbase: 1820mmX2050mm
• Maximum load: 50Kg
• Maximum range: 200km
• Maximum flight time: 240 minutes
• Working temperature:- 20℃~55℃
• Storage temperature:- 25℃~65℃
• Power mode: Oil electric hybrid
Characteristic:
• Oil electric hybrid, high load capacity, long endurance, low temperature resistance, low
noise;
• Vertical takeoff and landing, easy to operate,simple maintenance, and high cost-effectiveness;
• Capable of mounting multiple types of strike weapons and communication equipment, with a load module designed for quick disassembly within 1 minute;
• New folding design for easy transportation of micro vehicles;
• Capable of cluster flight (5 aircraft).
The BG-Q700 is a hybrid-powered tiltrotor unmanned aerial vehicle (UAV). It features rotors arranged at the wingtips that can tilt along with the nacelles. It simultaneously has the characteristics of a helicopter, such as vertical takeoff and landing and hovering in the air, as well as those of a fixed-wing aircraft, including high-speed cruising and a long flight range.The BG-Q700 adopts a high-lift thick airfoil, a moderate aspect ratio, and a straight wing without sweepback. This wing design provides a large lift force, a good lift-to-drag ratio during cruising and climbing, and excellent stiffness characteristics. Its structural design and manufacturing process are simple, and it has good maintainability.It has the capability of taking off and landing on the plateau and cruising at high altitudes. Through the expandable mission cabin and the fuselage with external suspension capability, as well as the skid-type landing gear, it can meet different mission requirements.
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