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
20kg
Maximum payload
122 m/h
Never Exceed Speed
5200m
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: about 3500-4200g (depending on custom strength).
Maximum take-off weight: 40 kg.
Maximum payload: 20kg (standard: 5kg) | Duration: 105 min@1kg load/60 min@6kg |
Maximum load life: 2H (123 min)@18kg-7m/s | Maximum control range: remote manual control/about 0.5 KM-1 km, ground station/5 KM-60 km |
Standard cruising speed: 7M/s@18.5 kg | Maximum cruising speed: 15 m/s (54 km/h) |
Never Exceed Speed: 122 m/h (about 34 m/s) | Standard battery size: 22.8 V/25AH * 4(45.6 V) |
Maximum level flight altitude: 5200m | Wind Resistance: no less than Force 5(Gust 6) |
Take-off and landing maximum wind resistance: no less than 4 wind (Gust 5) | Power blade size: 28-30 inches (recommended) |
Minimum thrust-to-weight ratio for safety: 1.3 | Plateau performance: passed the Plateau Test (plateau standard power configuration please contact the manufacturer to obtain) |
Standard no-load take-off weight: approximately 18 kg | Safety voltage on approach: not less than 43.8 V (Grignard high voltage battery) |
Arm mounting angle: 0 ° | Does the system support power-off |
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