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TD220 Coaxial Unmanned Helicopter

The United Aircraft TD220 Coaxial Unmanned Helicopter is a compact utility platform with a coaxial dual-rotor layout, autonomous flight functions and three payload suspension points. Designed for powerline inspection, disaster relief support and aerial mapping, it offers a 100 km operating radius and flight duration of 5 h with a 35 kg payload.

United AircraftAgricultural drone
Maximum endurance
Up to 6 hours.

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Product overview

The United Aircraft TD220 Coaxial Unmanned Helicopter is a small utility platform for powerline inspection, disaster relief support and aerial mapping. Its compact coaxial dual-rotor layout supports take-off and landing in small fields. Three general-purpose suspension points at the nose and fuselage accommodate different mission payloads, including an EO pod, communication relay equipment, SAR, weapons and military supplies. Electronic individual rotor control and an H∞ control algorithm provide adaptive flight control, while integrated navigation combines multiple sources.

The TD220 has a maximum take-off weight of 350 kg, a service ceiling of 3500 m, a maximum level speed of 100 km/h and an operating radius of 100 km. Endurance reaches up to 6 hours, with flight durations of 5 h carrying 35 kg and more than 4 h carrying 60 kg. Wind resistance is force 6 (12 m/sec). Autonomous functions cover take-off, landing, preset-course flight, online course planning, return to base, and status monitoring and warning.

Surveying & inspectionFire & rescue

Specifications

TD220 Coaxial Unmanned Helicopter specifications
SpecificationValue & conditions
Product typeUnited Aircraft TD220 Coaxial Unmanned Helicopter; small utility unmanned helicopter platform.
Rotor layoutCoaxial dual-rotor layout.
Payload attachment pointsThree general-purpose suspension points at the nose and fuselage.
Loadable payloadsEO pod, communication relay equipment, SAR, weapons and military supplies.
Maximum take-off weight350 kg.
Service ceiling3500 m.
Maximum level speed100 km/h.
Operating radius100 km.
Flight duration with 35 kg payload5 h.Payload of 35 kg.
Flight duration with 60 kg payloadGreater than 4 h.Payload of 60 kg.
Maximum enduranceUp to 6 hours.
Wind resistanceWind force 6 (12 m/sec).
Rotor controlElectronic individual rotor control with an H∞ control algorithm.
Navigation redundancyMulti-source fusion navigation maintains safety if one sensor fails.Failure of one sensor.
Emergency returnAutomatic return to base supported by system self-monitoring and emergency safety policies.Satellite shielding and data link interruption.
Autonomous functionsFully autonomous take-off and landing, preset-course flight, online course planning, one-key autonomous return to base, and autonomous status monitoring and warning.
ApplicationsPowerline inspection, disaster relief support and aerial mapping.

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