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T1400 Tandem Unmanned Helicopter

The United Aircraft T1400 Tandem Unmanned Helicopter is a twin-engine, heavy-lift platform designed for plateau operations and high-altitude takeoff and landing. Its internal cargo compartment, external suspension connector and autonomous flight functions support logistics, emergency rescue, agricultural protection, firefighting and communication support, with endurance of ≥8 hours carrying a 200 kg payload.

United AircraftAgricultural drone
Maximum payload capacity
650 kg
Dimensions
6.65 × 1.32 × 2.85 m

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Product overview

The United Aircraft T1400 Tandem Unmanned Helicopter combines a tandem rotor configuration with two engines, a multiple redundant flight control system and a combined navigation system. If one engine fails, the remaining engine can drive both the front and rear rotors. Autonomous functions include takeoff and landing, obstacle avoidance, spot hovering and precise delivery. An internal cargo compartment and an external suspension connector support transport of people and cargo, with applications spanning material delivery, communication support, agricultural protection, fire extinguishing and emergency rescue.

The T1400 measures 6.65 × 1.32 × 2.85 m (L × W × H) and has a maximum takeoff weight of 1400 kg. Maximum payload capacity is 650 kg with fuel. Endurance is ≥2 hours with a 500 kg payload and ≥8 hours with a 200 kg payload. Maximum horizontal flight speed is 180 km/h, cruising speed is 120 km/h, and the typical mission radius is 200 km, expandable. Its service ceiling is 6500 m, with a maximum takeoff and landing height of 5000 m.

Designed for high-altitude regions, the T1400 operates from -40°C to 55°C, provides rain protection for moderate rain and has takeoff and landing wind resistance of ≥13.9 m/s (level 7). It can carry EO pods, megaphones, searchlights, HD mapping equipment, communication relay devices, rescue equipment, spraying devices, firefighting devices and transportation suspension equipment. Stretchers, oxygen machines and infusion devices can be integrated into the cargo compartment, which can also carry medical staff for medical transport missions.

AgricultureSurveying & inspectionCargo & deliveryFire & rescue

Specifications

T1400 Tandem Unmanned Helicopter specifications
SpecificationValue & conditions
Product type and configurationT1400 heavy-lift tandem-rotor unmanned helicopter designed for plateau operations and high-altitude takeoff and landing.
Flight control and navigationMultiple redundant flight control system and combined navigation system.
Twin-engine rotor driveTwo engines; either remaining engine can drive both front and rear rotors following a single engine failure.In the event of a single engine failure.
Cargo handlingInternal cargo compartment and external suspension connector support trans-regional logistics and transport of people and cargo.
Autonomous flight functionsAutonomous takeoff and landing, obstacle avoidance, spot hovering and precise delivery.
Supported mission payloadsCan carry EO pods, megaphones, searchlights, HD mapping equipment, communication relay devices, rescue equipment, spraying devices, firefighting devices and transportation suspension equipment.
Medical transport equipmentCargo compartment can accommodate integrated stretchers, oxygen machines and infusion devices, and can carry medical staff.When integrated into the cargo compartment.
ApplicationsCommunication support, material transport and delivery, agricultural protection, fire extinguishing and emergency rescue.
Dimensions6.65 × 1.32 × 2.85 mL × W × H.
Maximum takeoff weight1400 kg
Endurance with 500 kg payload≥ 2hPayload of 500 kg.
Endurance with 200 kg payload≥ 8hPayload of 200 kg.
Maximum payload capacity650 kgWith fuel.
Service ceiling6500 m
Typical mission radius200 kmExpandable.
Maximum horizontal flight speed180km/h
Cruising speed120km/h
Maximum takeoff and landing height5000 m
Wind resistance≥13.9 m/s (level 7)During take-off and landing.
Operating temperature-40°C to 55°C
Rainproof capabilityModerate rain

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