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AVIC AR500C Unmanned Plateau Helicopter

SKU: MD-P00537·UAV Platforms·Made to Order

AVIC AR500C Unmanned Plateau Helicopter
AVIC AR500C Unmanned Plateau Helicopter
AVIC AR500C Unmanned Plateau Helicopter

Overview

Chinese aero-industry has full-embraced the concept of indigenous Unmanned Aerial System (UAS) design and development. This goes beyond the typical short- and medium-altitude fixed-wing performers and now includes unmanned rotorcraft such as the AR-500C by aviation Industry Corporation (AVIC) of China. The helicopter completed its maiden 20-minute-long flight in May of 2020 and continues development as of this writing. The AR-500C is built atop the proven framework of the earlier AR-500B model and, once operational, will be tasked with high-altitude reconnaissance work, suitable for operating in the "hot-and-high" rugged mountainous areas of China. Development work began in 2019 with the first flyable example completed in March of 2020. Ground-testing commenced soon after leading up to the first-flight in May. As an unmanned rotorcraft, the AR-500C takes on a conventional design shape with the main rotor mast set above the fuselage and the tail rotor unit (facing port side) installed at the extreme end of the tail stem as an anti-torque solution. The tail unit also incorporates vertical fins and a curved skid rod. The fuselage of the helicopter houses all pertinent mission and operational systems with a traversing optics set at the "chin" position - providing unfettered, real-time views of the action ahead and surrounding the helicopter. For ground-running, the vehicle is equipped with a simple four-point landing skin solution. Beyond its intended general reconnaissance role, developers of the AR-500C envision a slew of over-land / over-battlefield roles for their helicopter design including NBC (Nuclear-Biological-Chemical) data-collection, humanitarian aid, Search and Rescue (SAR), maritime patrol, and Electronic Warfare (EW). Maximum cruising speed: 165 km/h Maximum take-off weight: 500kg

Technical specification

Specifications. Key specifications: Maximum cruising speed 165 km/h, Maximum take-off weight 500kg, Endurance 5 hours, Maximum take-off altitude 5000 meters, Use ceiling 6700 meters.

Technical specification — 1 groups
Key specifications: Maximum cruising speed 165 km/h, Maximum take-off weight 500kg, Endurance 5 hours, Maximum take-off altitude 5000 meters, Use ceiling 6700 meters.

Technical specifications

Specifications

Maximum cruising speed
165 km/h
Maximum take-off weight
500kg
Endurance
5 hours
Maximum take-off altitude
5000 meters
Use ceiling
6700 meters

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