Alpin VTOL UAS has been created in accordance with the needs and requirements of the Turkish Rescue & Security industry. The Alpin UAS is a long-range, heavy-lift unmanned helicopter capable of carrying up to 160 kg with a range of up to 840 km. The converted Alpin UAS is based on the piloted Heli-Sport Italian CH7 helicopter.
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
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 |
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 |
Phone: +1 650 584-3176
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