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RONGQE INTELLIGENCE KTX3

By RONGQE INTELLIGENCE ↗

The RONGQE INTELLIGENCE KTX3 is a four-axis, eight-rotor heavy-lift UAV for pickup-supported firefighting. Under standard laboratory test conditions, maximum payload is 200 kg and endurance is 55 minutes unloaded or 14 minutes fully loaded. Vehicle integration provides a dedicated landing platform, mechanical securing, water supply and battery replenishment.

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RONGQE INTELLIGENCE KTX3 drone with a red body and black rotors in front of a burning building
RONGQE INTELLIGENCE KTX3 drone with a red body and black rotors in front of a burning building
Maximum payload200 kgLaboratory result under standard test conditions.
Unloaded endurance55 minutesUnloaded; laboratory result under standard test conditions.
Aircraft architectureHeavy-lift flight platform with four rotor axes and eight rotors.
Full-load endurance14 minutesFully loaded; laboratory result under standard test conditions.
PositioningOptional centimeter-level RTK positioning.Optional RTK equipment; technical parameters obtained under standard laboratory test conditions.
Vehicle landing interfaceDirect landing on the dedicated platform above the pickup bed, with rapid securing by mechanical latches.Firefighting pickup equipped with the dedicated takeoff and landing platform.

Product overview

The RONGQE INTELLIGENCE KTX3 is a heavy-lift flight platform with four rotor axes and eight rotors, intended for pickup-supported firefighting using an aircraft-mounted water gun. Its maximum payload is 200 kg, with endurance of 55 minutes unloaded and 14 minutes fully loaded under standard laboratory test conditions. Payload therefore materially affects flight duration. Centimeter-level RTK positioning is optional. Flight environment, mission payload, operation, maintenance and software version can affect actual performance.

The aircraft can land directly on a dedicated platform above the firefighting pickup bed and be secured quickly with mechanical latches. The associated pickup incorporates a 1.34-tonne self-contained water tank and high-pressure pump to supply the airborne water gun continuously. Under standard laboratory test conditions, pickup energy storage supports 2–3 aircraft battery replenishments taking 20–30 minutes each, while the complete system takes no more than 3 minutes from pickup positioning to the first aircraft becoming airborne.

Specifications

SpecificationValue & conditions
Aircraft architectureHeavy-lift flight platform with four rotor axes and eight rotors.
Maximum payload200 kgLaboratory result under standard test conditions.
Unloaded endurance55 minutesUnloaded; laboratory result under standard test conditions.
Full-load endurance14 minutesFully loaded; laboratory result under standard test conditions.
PositioningOptional centimeter-level RTK positioning.Optional RTK equipment; technical parameters obtained under standard laboratory test conditions.
Vehicle landing interfaceDirect landing on the dedicated platform above the pickup bed, with rapid securing by mechanical latches.Firefighting pickup equipped with the dedicated takeoff and landing platform.
Water tankBuilt-in 1.34-tonne self-contained water tank.Associated pickup configuration.
Water deliveryPickup-mounted high-pressure pump provides continuous water supply to the aircraft-mounted water gun.Associated pickup supplying the aircraft-mounted water gun.
Battery replenishment capacity2–3 UAV battery replenishments.Using the pickup's stored energy; laboratory result under standard test conditions.
Battery replenishment time20–30 minutes per replenishment.Each battery replenishment using the pickup's stored energy; laboratory result under standard test conditions.
System deployment timeNo more than 3 minutes.Complete pickup-based system, from pickup positioning to the first UAV becoming airborne; laboratory result under standard test conditions.
Performance measurement conditionsStandard laboratory test conditions; actual performance can vary with flight environment, mission payload, operation, maintenance and software version.Technical parameters and performance figures measured under standard laboratory test conditions; flight environment, mission payload, operation, maintenance and software version can affect actual performance.

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