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
5KG
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: 5800g (depending on custom strength).
Maximum take-off weight: 15.5 kg.
Parameter | Value |
|---|---|
Model | H5-1 |
Produt material | Carbonfber integrated frame |
Number of rotors | 4 rotors |
Whelbase | ≤1030mm |
Unfolded size (mm) | 810*810*470mm(±20mm) |
Empty welght | 55.8KG(excluding batery weight) |
Maximum load | 55KG |
Maximum takeff weight | ≤15.5KG |
Maximumfight speed | ≤18m/s |
Maximumascent speed | ≤5m/s |
Maximum descent speed | ≤4m/s |
Maximum takeoffaltitude | 3000m |
Unloaded endurance | 260min |
5kg endurance | 230min |
Positioning system | GPSpositioning |
Power system | High-efcienecy FOC power |
Propeller size | 24-inch folding propellers |
Power battery | 6S27000mAh*2 |
Charger | lntligent superfatcharging |
Remote control | 1920*1080 integrated display 5.5-inch screen |
Remote control standby time | 3-5 hours |
Image and data transmision distance | 5km(upgradeable) |
Safe wind speed | ≤6 levels |
Operating temperature | -20℃to 50℃ |
Fuselage protection level | IP54 |
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