Body material: carbon fiber, aviation aluminum alloy, injection molded parts, etc.
Landing gear mounting position: under the fuselage
Mission module location: inside the airframe
Body material: carbon fiber, aviation aluminum alloy, injection molded parts, etc.
Landing gear mounting position: under the fuselage
Mission module location: inside the airframe
10KG
Maximum payload
18m/s
Never Exceed Speed
3000m
Maximum level flight altitude
0°
Arm mounting angle
Body material: carbon fiber, aviation aluminum alloy, injection molded parts, etc.
Landing gear mounting position: under the fuselage.
Mission module location: inside the airframe.
Structure weight: 8800g (depending on custom strength).
Maximum take-off weight: 36 kg.
Parameter | Specification |
|---|---|
Model | H10-1 |
Material | Carbon Fiber + Aviation Aluminum Alloy |
Number of Rotors | 6 |
Wheelbase | ≤1630mm (±20mm) |
Unfolded Size | 1730×1510×600mm (±20mm) |
Empty Weight | ≤8.8KG (excluding battery) |
Maximum Payload | ≤10KG |
Maximum Takeoff Weight | ≤36KG |
Maximum Flight Speed | ≤18m/s |
Maximum Ascent Speed | ≤5m/s |
Maximum Descent Speed | ≤4m/s |
Maximum Takeoff Altitude | 3000m |
Endurance (No Load) | ≥80min |
Endurance (10kg Load) | ≥40min |
Positioning System | RTK+GPS |
Power System | High-Efficiency FOC |
Propeller Size | 30-inch Carbon Fiber (Straight Blade) |
Power Battery | 12S 32000mAh×2 |
Charger | Intelligent Super Fast Charging |
Remote Control | 7" Integrated Display (1920×1080) |
Remote Standby Time | 8-15 hours |
Transmission Distance | 10km (Upgradable) |
Max Wind Resistance | ≤Level 6 |
Operating Temperature | -20℃ to 50℃ |
Protection Level | IP54 |
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