Product overview
The JIUSI D40 is a multifunction transport UAV with a maximum payload of 40kg. Its all-carbon-fiber body uses a modular quick-release structure with four detachable arms, with deployment taking 3 minutes. An included active cargo-release function lets operators remotely control release timing and place cargo at a designated target. The aircraft also supports two controllers: pilots at separate locations can transfer control authority with one button. These features combine a detachable physical architecture with remotely operated cargo delivery and control handover.
The standard battery configuration is 18S62000mah for 30KG long-distance transport, while the optional 18S41000mah configuration is intended for 40KG short-distance transport. Built-in dual redundant RTK modules are standard equipment. Radar and visual obstacle sensors provide real-time information about surrounding obstacles. The controller has a 7-inch high-brightness screen, an 8-core processor and a manual operating mode. Motor cooling uses a centrifugal air-cooling system with an integrated heat-dissipation array. The aircraft has an IP55 protection rating and corrosion resistance.
Communication distance varies with flight height and signal conditions. At a flight height of 3–6m, communication distance is 3–6KM. At 120m with low obstruction and moderate interference, the distance is 10–15KM; at the same height with no obstruction and low interference, it is 30–40KM. These distances retain their respective height, obstruction and interference conditions. The D40 also has a Force 7 wind-resistance rating. Its battery configurations distinguish standard 30KG long-distance transport from optional 40KG short-distance transport.
Specifications
| Specification | Value & conditions |
|---|---|
| Model | D40 |
| Unfolded dimensions | 2910mm × 3050mm × 860mmUnfolded configuration. |
| Maximum wheelbase | 2200mm |
| Maximum takeoff weight | 90.1kg |
| Hovering accuracy | Vertical ±0.1m; horizontal ±0.1m |
| Maximum hovering time, unloaded | 50minUnloaded. |
| Maximum hovering time, 40KG load | 21minFull load of 40KG. |
| Maximum hovering time, 30KG load | 27minFull load of 30KG. |
| Maximum flight distance, unloaded | 45kmUnloaded. |
| Maximum flight distance, 40KG load | 18.5kmFull load of 40KG. |
| Maximum wind speed tolerated | 12m/s |
| Maximum horizontal flight speed | 15m/s |
| Maximum flight altitude above sea level | 4500m |
| Operating ambient temperature | -10°C to 45°C |
| Battery capacity | 62000mah |
| Empty aircraft weight | 35kg without battery; 50.1kg with battery35kg excludes the battery; 50.1kg includes the battery. |
| Remote control distance | 5-40km |
| Operating frequency | 5.8GHz/2.4GHz |
| Remote controller operating time | 8 hours |
| Camera pod resolution and sensor size | 4 million pixels; 1/2.7-inch sensor |
| Product type | Multifunction transport UAV |
| Maximum payload | 40kg |
| Wind resistance rating | Force 7 |
| Communication distance at low flight height | 3–6KMFlight height 3–6m. |
| Communication distance with moderate interference | 10–15KMFlight height 120m; low obstruction and moderate interference. |
| Communication distance with unobstructed signal | 30–40KMFlight height 120m; no obstruction and low interference. |
| Environmental protection | IP55 protection rating and corrosion resistance |
| Positioning equipment | Dual redundant RTK modulesBuilt-in standard equipment. |
| Standard battery configuration | 18S62000mah30KG long-distance transport; standard configuration. |
| Optional battery configuration | 18S41000mah40KG short-distance transport; optional configuration. |
| Motor cooling | Centrifugal air cooling with an integrated heat-dissipation array |
| Controller display | 7-inch high-brightness screen |
| Controller processor | 8-core processor |
| Manual control | Manual operating mode |
| Airframe architecture | Modular quick-release structure with four detachable arms |
| Airframe material | All-carbon-fiber body |
| Deployment time | 3 minutes |
| Payload release | Included active release function with remotely controlled release timing |
| Dual-controller operation | One aircraft supports two controllers with one-button transfer of control authorityTwo pilots at separate locations. |
| Obstacle sensing | Radar and visual sensors for real-time obstacle detection |
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