R22-UV

Based on Robinson R22.
Take-off, en-route flight and landing
are fully automatic

Overview

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 dropping up to 180 kg (400 lbs) at specified location
  • Radio relay
  • Agricultural operations using spraying equipment
  • Flying R&D laboratory (meteorology, hydrology, earth monitoring, etc.)

OPERATION SPECIFICATIONS

Parameters Data
Level surface 15m x 15m
Control modes:
Main
Assisted
Emergency situations
Fully automatic
Semi-automatic
Emergency
Takeoff and landing Fully automatic
Emergency landing Autorotation
Ground support equipment Not required
Engine start Automatic

 

TECHNICAL SPECIFICATIONS

Parameters Data
Maximum cruising speed 160 km/h
Maximum speed 189 km/h
Cruise fuel consumption l/h 33.5
Length 8800 mm
Main rotor diameter 7700 mm
Height 2700 mm
Wheelbase 1800 mm
Engine type Four-stroke engine
Engine Lycoming O-320-A2B
Engine power 124 HP
Fuel tank capacity 270 l
Payload with full fuel tank 40 kg
Max. takeoff weight 635 kg
Max. climbing rate 6 m/s
Max. wind speed during taking off or landing 14 m/s
Operational range 1020 km
Service ceiling 4200 m
Endurance 6 h
Generator / starter (output DC) 25A 28V
Onboard power supply 28V
Autorotation Yes
Altimeter radio
TBO 2200 h

 

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