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COMMERCIAL AIRCRAFT

Cableway C-400

By Zhejiang Cableway Aerospace Technblogy Go., Ltd ↗

The Zhejiang Cableway Aerospace C-400 is a heavy-lift multirotor for mountain engineering and transport. Its eight-axis, sixteen-propeller configuration carries a 320 kg standard payload or 400 kg maximum payload. Endurance is 8 minutes at standard load. Eight batteries and a standard weighing system define its configuration, with landing and obstacle-avoidance radars optional.

Maximum payload400 kg
Maximum takeoff weight700 kg
Unladen endurance25 minutesUnladen.
Cruise speed10 m/s
Aircraft architectureEight axes with sixteen propellers
Battery configuration8 batteries

Product overview

The Zhejiang Cableway Aerospace C-400 is a heavy-lift multirotor flight platform for mountain engineering and transport. Its physical architecture uses eight axes and sixteen propellers, with deployed dimensions of 490 × 490 × 65 cm and stowed dimensions of 210 × 210 × 200 cm. Aircraft weight is 190 kg excluding batteries. It carries a standard payload of 320 kg and a maximum payload of 400 kg, with a maximum takeoff weight of 700 kg.

The aircraft uses eight batteries with an energy capacity of at least 20 kWh. Endurance is 25 minutes unladen or 8 minutes carrying the standard 320 kg payload. Charging time is 15 minutes per set with four fast chargers, and the charging ambient temperature range is -10°C to 45°C. A weighing system is standard equipment. Landing-assistance radar and front/rear obstacle-avoidance radar are optional equipment, so these functions depend on the selected aircraft configuration.

Cruise speed is 10 m/s, maximum horizontal speed is 20 m/s, and maximum ascent/descent speed is 8 m/s. Communication distance is 30 km with line of sight and no interference. Wind resistance is Level 7, while operating temperature spans -20°C to 55°C. The flight ceiling is ≤3000 m. With high-altitude propellers fitted, maximum operating altitude has conflicting ratings of ≥4500 m and ≤4500 m; the propeller requirement applies to both figures.

Specifications

SpecificationValue & conditions
Aircraft architectureEight axes with sixteen propellers
Battery configuration8 batteries
Deployed dimensions490 × 490 × 65 cm
Stowed dimensions210 × 210 × 200 cm
Aircraft weight190 kgExcluding batteries.
Maximum payload400 kg
Maximum takeoff weight700 kg
Standard payload320 kg
Unladen endurance25 minutesUnladen.
Loaded endurance8 minutesStandard payload of 320 kg.
Charging time15 minutes per setFour fast chargers.
Battery energy capacity≥20 kWh
Wind resistanceLevel 7
Charging ambient temperature-10°C to 45°CDuring charging.
Maximum horizontal speed20 m/s
Maximum ascent/descent speed8 m/s
Cruise speed10 m/s
Weighing systemIncluded as standardStandard equipment.
Flight ceiling≤3000 m
Communication distance30 kmLine of sight, without interference.
Maximum operating altitude≥4500 mEquipped with high-altitude propellers.
Maximum operating altitude, detailed specification≤4500 mEquipped with high-altitude propellers.
Operating temperature-20°C to 55°CDuring operation.
Radar optionsLanding-assistance radar and front/rear obstacle-avoidance radarOptional equipment.
Intended applicationMountain engineering and transport
Manufacturer and modelZhejiang Cableway Aerospace C-400

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