UVH-500 (KAHU-150)
VTOL UAS
ADVANTAGES
Night operations and flights under severe weather conditions
All terrain capable
Primed for ease operations
Meeting operational requirements
Low life cycle costs
Remote Ground Controls network capability
Simultaneous multi-UAV operation
Customizable software and SDK
Auto-rotation landing capability and high efficiency flight control, based on TECS
Redundant autopilot system
Payload Options:
- EO/IR
- RADARS SAR/GMTI
- LIDAR
- HYPERSPECTRAL
APPLICATION
- Video surveillance and monitoring
- Autonomous cargo transportation and delivery
- Cargo delivery up to 140 kg payload with a range of 100 km
- Radio relay
- Agricultural operations using spraying equipment
- Flying R&D laboratory (meteorology, hydrology, earth monitoring, etc.)
PERFORMANCE
Parameters | Data |
|---|---|
Maximum cruising speed | 160 km/h |
VNE | 209 km/h |
MTOW | 500 kg |
Max. Payload (including fuel): | 160 kg |
Rate of Climb | 5 m/s |
Max. Range (cruising speed 120 km/h) | 840 km |
Max. Operating Altitude | 5000 m |
Flight time (max.) Payload - 20 kg | 7 h |
Flight time (max.) Payload - 120 kg | 2 h |
PHYSICAL SPECIFICATIONS
Parameters | Data |
|---|---|
Main rotor diameter | 6280 mm |
Airframe lenght | 7050 mm |
Height | 2350 mm |
Wheelbase | 1500 mm |
Empty weight | 340 kg |
Engine type | Rotax 914 UL |
Engine capacity | 115 HP |
Fuel tank | 180 liter / 135 kg |
Horizontal flight fuel consumption / h | 25 liter / 18.6 kg |
Max. wind speed during takeoff or landing | 14 m/s |
Onboard power supply | 12V/24V |
Altimeter | Radio |
Transponder with ADS‐B | S |
TBI (inspections, maintenance) | 100 h |
Overhaul | 1200 h |
Hovering IGE (ISA) | 3500 m |
Hovering OGE (ISA) | 2500 m |
