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Zhejiang Cableway Aerospace Technblogy Go., Ltd C-1000

By Zhejiang Cableway Aerospace Technblogy Go., Ltd ↗

The Zhejiang Cableway Aerospace Technblogy Go., Ltd C-1000 is a six-axis, twelve-propeller heavy-lift UAV for mountain engineering and transport. It has a 500 kg standard payload, 1000 kg maximum payload and 2000 kg maximum takeoff weight. Fast-charge battery endurance is 20 minutes unladen or 8 minutes loaded.

Maximum payload1000 kg
Maximum takeoff weight2000 kg
Unladen endurance20 minUnladen; fast-charge battery.
Cruise speed10 m/s
Product identityZhejiang Cableway Aerospace Technblogy Go., Ltd C-1000
Intended applicationsMountain engineering and transport

Product overview

The Zhejiang Cableway Aerospace Technblogy Go., Ltd C-1000 is a heavy-lift multirotor aircraft for mountain engineering and transport. Its six-axis structure carries twelve propellers, with deployed dimensions of 755 × 656 × 65 cm and stowed dimensions of 210 × 210 × 230 cm. These define its operating and storage footprint; payload accommodation is expressed through a 500 kg standard load and 1000 kg maximum load. Maximum takeoff weight is 2000 kg, a separate limit from its payload capacity.

The battery-powered platform has a capacity of ≥28 kWh and a charging time of 15 minutes per set using a fast-charging station. With fast-charge batteries, endurance is 20 minutes unladen and 8 minutes loaded, without a specified load mass for that endurance figure. Cruise speed is 10 m/s, maximum horizontal speed is 20 m/s, and maximum climb/descent speed is 8 m/s. Communication extends to 10 km under interference-free, line-of-sight conditions. Operating temperature spans -20°C to 55°C, with Level 7 wind resistance. Maximum operating altitude is ≥3500 m with high-altitude propellers; the separate flight-ceiling specification is ≤3000 m.

Specifications

SpecificationValue & conditions
Product identityZhejiang Cableway Aerospace Technblogy Go., Ltd C-1000
Intended applicationsMountain engineering and transport
Aircraft architectureSix-axis, twelve-propeller multirotor
Deployed dimensions755 × 656 × 65 cm
Stowed dimensions210 × 210 × 230 cm
Maximum payload1000 kg
Maximum takeoff weight2000 kg
Standard payload500 kg
Maximum operating altitude≥3500 mEquipped with high-altitude propellers.
Flight ceiling≤3000 m
Unladen endurance20 minUnladen; fast-charge battery.
Loaded endurance8 minLoaded; fast-charge battery.
Wind resistanceLevel 7
Operating temperature-20°C to 55°C
Communication distance10 kmLine of sight; no interference.
Cruise speed10 m/s
Maximum horizontal speed20 m/s
Maximum climb/descent speed8 m/s
Battery capacity≥28 kWh
Charging time15 minutes per setUsing a fast-charging station.

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