| Product identity | Spider-iUAV M400 heavy-lift transport drone |
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| Applications | Cargo transport, aerial firefighting, infrastructure inspection, emergency rescue and commercial logistics |
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| Aircraft type | Octocopter (8-Axis)Technical specifications are theoretical values based on ideal-condition tests; actual operation may vary. |
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| Construction material | Aviation-grade carbon fiberTechnical specifications are theoretical values based on ideal-condition tests; actual operation may vary. |
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| Dimensions | 4400 x 4400 x 1005 mmUnfolded; theoretical specification based on ideal-condition tests; actual operation may vary. |
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| Folded size | 1.4×1.1mFolded for storage. |
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| Payload capacity | Rated payload: 150kg; peak lift capacity: 200kg |
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| Maximum takeoff weight | 333kgTheoretical value based on ideal-condition tests; actual operation may vary. |
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| Power system | Solid-state batteryTechnical specifications are theoretical values based on ideal-condition tests; actual operation may vary. |
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| Multi-mission payload rack | Change the tripod for rapid deploymentTechnical specifications are theoretical values based on ideal-condition tests; actual operation may vary. |
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| Cruise speed | 20 km/hCruise; theoretical value based on ideal-condition tests; actual operation may vary. |
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| Flight radius | 10kmTheoretical value based on ideal-condition tests; actual operation may vary. |
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| Altitude limit | 5kmTheoretical value based on ideal-condition tests; actual operation may vary. |
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| Engine and frame lifespan | Engine: 100,000 hours; frame: ≥10 yearsTheoretical values based on ideal-condition tests; actual operation may vary. |
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| Wind resistance | Level 7Theoretical value based on ideal-condition tests; actual operation may vary. |
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| Hovering and flight modes | Omnidirectional hovering; manual, intelligent and automatic modesTechnical specifications are theoretical values based on ideal-condition tests; actual operation may vary. |
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| Navigation functions | Automatic altitude, position hold, return, AB point memory and autonomous planningTechnical specifications are theoretical values based on ideal-condition tests; actual operation may vary. |
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| Night flight | SupportedTechnical specifications are theoretical values based on ideal-condition tests; actual operation may vary. |
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| Safety and recording equipment | Electronic fencing and flight data recorderTechnical specifications are theoretical values based on ideal-condition tests; actual operation may vary. |
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| Obstacle sensing and flight precision | 360° obstacle sensing; centimeter-level precision for autonomous flightsRadar and RTK fusion during autonomous flight. |
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| Rotor arrangement | Coaxial dual rotors with counter-rotating propellers |
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| Blade construction | Lightweight, heat-resistant carbon fiber blades |
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| Flight automation | One-tap return-to-home, waypoint resume and automatic failsafe |
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| Anti-sway stabilization | Onboard flight-controller algorithms detect and suppress pendulum oscillation in real timeDuring lifting. |
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| Payload release | Hook mechanism with automatic and manual quick release |
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| Fleet coordination capacity | Up to 30 unitsCoordinated swarm airlifts. |
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| Pilot handover | Instant one-tap pilot handoverMaster-slave dual-pilot control. |
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| Spare-parts standardization | 90% cross-compatible spare parts |
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| Technical specification measurement basis | Technical parameters are theoretical values from ideal-condition tests; actual operating results vary with circumstances.Tests conducted under ideal conditions. |
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| Training and technical support | Comprehensive flight training, maintenance and 24/7 online support |
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