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.)

OPERATIONS 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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