JunFeng motor focused on vehicle development and core components for smart and new energy vehicles. Product development, innovative business models with the Internet + thinking way, explore new paths for the development of smart and new energy vehicles .
JF-XX300 (2025 model)
JunFeng motor focused on vehicle development and core components for smart and new energy vehicles. Product development, innovative business models with the Internet + thinking way, explore new paths for the development of smart and new energy vehicles .
JunFeng motor focused on vehicle development and core components for smart and new energy vehicles. Product development, innovative business models with the Internet + thinking way, explore new paths for the development of smart and new energy vehicles .
JF-XX300 (2025 model)
JF-XX300 Hybrid Multi-rotor UAV
The JF-XX300 Hybrid Multi-rotor UAV adopts a six-axis and six-propeller configuration as well as an environment-resistant design. It is equipped with fully automatic take-off and landing functions, and features extremely high flexibility, military-grade stability, large payload capacity and high reliability. It is widely used in scenario-level fields such as emergency communications, emergency rescue, high-intensity lighting, reconnaissance and search, material delivery, geographical mapping, power/pipeline inspection, and land resource survey.
Technical Parameters
Parameter Item Specific Specification
Wheelbase 4000 mm
Unfolded Dimensions 2 × 2 × 1.1 m
Maximum Payload Capacity 300 kg
Maximum Take-off Weight 600 kg
Communication Range 20 km
Maximum Take-off Altitude 3000 m
Maximum Flight Speed 10 m/s
Wind Resistance Class Level 6
Deployment Time 2 min
The JF-XX300 Hybrid Multi-rotor UAV adopts a six-axis and six-propeller configuration as well as an environment-resistant design. It is equipped with fully automatic take-off and landing functions, and features extremely high flexibility, military-grade stability, large payload capacity and high reliability. It is widely used in scenario-level fields such as emergency communications, emergency rescue, high-intensity lighting, reconnaissance and search, material delivery, geographical mapping, power/pipeline inspection, and land resource survey.
Technical Parameters
Parameter Item Specific Specification
Wheelbase 4000 mm
Unfolded Dimensions 2 × 2 × 1.1 m
Maximum Payload Capacity 300 kg
Maximum Take-off Weight 600 kg
Communication Range 20 km
Maximum Take-off Altitude 3000 m
Maximum Flight Speed 10 m/s
Wind Resistance Class Level 6
Deployment Time 2 min
Endurance 60 min
Application Scenarios:
Detailed technical parameters: Please refer to CC_junfemg@163.com Request.
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