CUAV New VT240 Pro VTOL for mapping surveying inspection
Features
- Carbon Fiber Composite
- Push Back Motor
- Long battery life
- 310km Cruising Range
- Self-Developed
- Portable Transportation
- 2kg Payload
- Fast Disassembly Design
Model VT240 Pro
CUAV New VT240 Pro VTOL is a light electric vertical take-off and landing UAV. The fuselage is made of carbon fiber and Kevlar composite material, which has the characteristics of lightweight and high strength. Fluid design, perfect integration of aerodynamics, low flight resistance, battery life of up to 4 hours, cruising range up to 260km; detachable design, quick disassembly, reasonable folding, and storage design, allowing air transport boxes Smaller size, making operation and transportation more portable.
Integrates a powerful CUAV self-developed UAV solution, supports off-site takeoff and landing, moving platform and landing, GPS rejection, formation flight, and other functions. ArduPilot’s complete open-source source system supports secondary development.
Pushback Motor DesignHigh Efficiency and Good Vision
Pushback motor design with low KV large pitch propellers for higher motor efficiency without blocking the camera view
Efficient Tail Thruster Motor Design
Does not block the pod view
Quick Loading StructurePortable for Operation&Transportation
The fluid design of the Raelfy VT240 fuselage perfectly integrates aerodynamics, makes the small flight resistance, the battery life is up to 4 hours, and the cruising range can reach 260km.
Quick Loading StructurePortable for Operation&Transportation
The fuselage adopts a modular design, which can be quickly disassembled and assembled. The reasonable folding and storage design makes the air transport box smaller and more portable for both operation and transportation.
Self-developed Core SystemPowerful Features
Integrate powerful CUAV self-developed autopilot, communication linkRTK, airspeed sensor, etc, support remote takeoff and landing, moving platform takeoff and landing, terrain following, cluster formation, and other functions
Remote Takeoff and Landing
Moving Platform Takeoff and Lading
Terrain Following
Formation
CRTKIPs
Powerful Autopilot
High precision positioning RTK
SKYE
Ultra-long Range communication Link
Intelligent Temperature CompensationAirspeed Sensor
Carbon Fiber Composite FuselageLight Weight Strong
The fuselage is made of carbon fiber and Kevlar composite material, which is lightweight and high strength, so the UAV has a longer service life
and reduce
2kg PayloadVarious camerasah10r22are available
2kg payload, supporting a variety of cameras, adapting to more diverse application scenarios
Application Scenarios
Mapping
3D Modeling I Urban Planning I GeologicalExplorationLand title confirmation
Security
Security and firefightingAnti-smuggling Anti-drugAnti-crime and evilMaritime SupervisionEmergency Rescue
Inspection
Land and TransportationOil and Gas PipelinesEnvironmental Protection SupervisionWater SupervisionForestry Supervision
Scientific research
Scientific experimentTraining and educationSecondary developmentSubiect research
Logistics
Logistics Transportation I EmergencyMaterial Transportation
Agriculture
Precision Agriculture Ecological Protection Poppy patrol
Specification
Body material | Carbon fiber + Kevlar composite material |
Size | 2438x1300x376mm |
Max flying speed | 30m/s |
Economical cruising speed | 18m/s (65km/h) |
Stall speed | 14.5m/s@13kg |
Max cruising range | 310km |
Max payload | 2kg |
Wind resistance | Level 5 |
Take-off and landing mode | VTOL |
Power energy | Electric |
Positioning accuracy | Single point positioning: 1.5M RTK: 1CM+1PPM |
Flight controller | Standard CUAV Autopilot (optional) |
Communication distance | Subject to link data |
Customized/Optional | Autopilot, GNSS receiver, remote controller. mission payload, fuselage coating, waterproof design, remote ID, etc. |
Ground station | QGoundcontrol/Missionplanner/LGC |
Application | Surveying and mapping, Inspection, monitoring, public security, traffic, etc. |
*lt depends on take-off weight, battery capacity, weather environment and other factors |
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