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COMMERCIAL AIRCRAFT

Hercules M4-X13

By Yifei Zhineng ↗

The Yifei Zhineng Hercules M4-X13 is a folding quadrotor UAV with a 30kg maximum payload and dedicated underside integration space. Its standard configuration includes propulsion equipment, a controller, batteries and charging equipment. The carbon-fiber and aluminum structure supports deployment within five minutes, with maximum unloaded endurance of 70 minutes.

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Hercules M4-X13 quadrotor drone with tall skid landing gear and a white central body
Hercules M4-X13 quadrotor drone with tall skid landing gear and a white central body
Payload integration spaceReserved customization space beneath the aircraft for installing heavy equipment and other payloads
Maximum takeoff weight100kg
Maximum endurance70minUnloaded aircraft.
Cruise speedNo numerical value specified; unit shown as m/s
Aircraft architectureQuadrotor UAV
Structural materialsHigh-strength carbon fiber and aviation-grade aluminum alloy

Product overview

The Yifei Zhineng Hercules M4-X13 is a quadrotor platform for carrying heavy equipment and other mounted payloads. Its structure combines high-strength carbon fiber with aviation-grade aluminum alloy, while reserved space beneath the aircraft supports customized payload installation. The folding architecture allows deployment within five minutes. With propellers excluded, the aircraft measures 3028 × 3028 × 1037mm unfolded and 1000 × 947 × 1025mm folded, with a 2460mm wheelbase. Empty weight is 28kg without batteries; maximum payload is 30kg and maximum takeoff weight is 100kg.

The standard configuration supplies an airframe, remote controller, three 18S 40AH batteries, charging equipment, four motors, four propellers, installation tools, a custom wiring harness, documentation and a custom packaging case. Maximum endurance is 70 minutes when unloaded. Operating limits include an ambient temperature range of -20°C to 50°C, Level 6 wind resistance and IP54 protection. Horizontal hovering accuracy is ±0.5m under good satellite positioning conditions. Parameters can be customized, with the delivery contract determining the agreed configuration.

Specifications

SpecificationValue & conditions
Aircraft architectureQuadrotor UAV
Structural materialsHigh-strength carbon fiber and aviation-grade aluminum alloy
Deployment timeCan be unfolded for operation within 5 minutes
Payload integration spaceReserved customization space beneath the aircraft for installing heavy equipment and other payloads
Parameter customizationAircraft parameters can be customized; the delivery contract determines the agreed configuration
Wheelbase2460mm
Unfolded dimensions3028*3028*1037mmExcluding propeller blades.
Folded dimensions1000*947*1025mmExcluding propeller blades.
Maximum endurance70minUnloaded aircraft.
Empty aircraft weight28kgExcluding batteries.
Maximum payload30kg
Maximum takeoff weight100kg
Cruise speedNo numerical value specified; unit shown as m/s
Maximum horizontal flight speed18m/s
Maximum ascent speed5m/s
Maximum descent speed2.5m/s
Maximum flight radius15km
Maximum takeoff altitude5000m above sea level
Wind resistanceLevel 6
Ingress protectionIP54
Operating ambient temperature-20°C to 50°C
Maximum tilt angle28°
Horizontal hovering accuracy±0.5mGood satellite positioning conditions.
Airframe supplied1 Hercules M4-X13 airframe setStandard factory configuration.
Remote controller supplied1 remote controllerStandard factory configuration.
Batteries and charging equipment supplied3 power batteries, each 18S 40AH; 1 charging deviceStandard factory configuration.
Propulsion equipment supplied4 EF Motor motors and 4 EF Propeller propellers, in CW/CCW configurationsStandard factory configuration.
Installation equipment supplied1 installation toolkit and 1 custom onboard wiring harness setStandard factory configuration.
Documentation supplied1 documentation set comprising a certificate of conformity and operating instructionsStandard factory configuration.
Packaging supplied1 custom packaging caseStandard factory configuration.
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