Customization: | Available |
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Certification: | ISO9001, FCC, RoHS, CE |
Height: | High Altitude |
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The XT6-2700 adopts an integrated carbon fiber molding process, offering exceptional overall structural strength with a maximum payload capacity exceeding 50 kg. It can carry heavy equipment and emergency devices for high-altitude operations. With excellent product quality and environmental adaptability, it maintains stable flight performance even in high-altitude and high-temperature environments. This product is widely applicable in fields such as emergency rescue and short-distance material delivery.
Wheelbase | 2695 mm |
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Dimensions | Φ 3914 x 990 mm (unfolded) |
Weight | 30.32 kg (excluding battery) |
Maximum Takeoff Weight | 135 kg |
Recommended Propeller | Diameter/Pitch: 48 x 17.5 inch |
Supported Satellite Systems | BDS B1/B2, GPS L1/I2, GLONASS L/L2, GALILEO E1/E2, QZSS L1/L2 |
GNSS | Supported |
Positioning Accuracy (RMS) | Vertical: ±1 m (GNSS Single Point), ±0.8 m (DGPS), ±1.5 cm + 1 ppm (RTK) Horizontal: ±1.5 m (GNSS Single Point), ±1 m (DGPS), ±1.0 cm + 1 ppm (RTK) |
Orientation Accuracy (RMS) | 0.5° |
Maximum Ascend Speed | 4 m/s |
Maximum Descent Speed | 2 m/s |
Maximum Horizontal Speed | 15 m/s |
Maximum Flight Altitude | 4000 m |
Maximum Wind Resistance | 13 m/s (Grade 6 wind) |
Maximum Flight Duration | No Load: 80 min 30 kg Load: 56 min 50 kg Load: 40 min |
Maximum Payload Flight | 60 kg |
Protection/Rainproof Rating | IP54 / Light Rain |
Radar Detection Range | 1.5 m - 50 m |
Operating Temperature Range | -20°C to 55°C |