Product overview
The DJI EV50 is a cargo flight platform built around vertical takeoff and landing followed by fixed-wing cruise. Eight lift rotors and three cruise propulsors form its redundant propulsion architecture, while a large-span wing supports longer transport routes. Runway-free deployment suits operations that need to move between locations. Its maximum payload is 50 kg, and its 270 L wide-body cargo compartment provides space for different cargo combinations. The 150 km maximum range and 160 km/h maximum airspeed both apply to the unladen aircraft.
For transport and storage, two people can assemble or disassemble the EV50 without tools within five minutes. Its equipment includes a standard parachute, redundant pitot tubes with self-heating support, and automatic propeller locking. PSDK support provides an expansion route for mission equipment. During a May 2026 scientific mission from Everest Base Camp, an EV50 carrying an ozone measuring instrument and other equipment reached 8,861 m above sea level in thin, low-pressure air and complex winds; this figure describes that mission’s achieved altitude.
Specifications
| Specification | Value & conditions |
|---|---|
| Product identity and purpose | DJI EV50 vertical-takeoff-and-landing cargo UAV for cross-regional aerial transport over hundred-kilometre-scale distances. |
| Deployment | Vertical takeoff and landing without a runway. |
| Maximum range | 150 kmUnladen aircraft. |
| Maximum payload | 50 kg |
| Maximum flight airspeed | 160 km/hUnladen aircraft. |
| Cargo compartment | 270 L wide-body cargo compartment. |
| Propulsion architecture | Redundant propulsion system with eight rotors and three cruise propulsors. |
| Flight architecture | Eight-rotor vertical takeoff with three-propulsor cruise. |
| Wing configuration | Large-span wing for fixed-wing cruise. |
| Airspeed sensing | Redundant pitot-tube design with self-heating support. |
| Parachute | Parachute included as standard.Standard equipment. |
| Propeller locking | Automatic propeller-locking function. |
| Assembly and disassembly | Within 5 minutes.Two-person team; no tools. |
| Payload integration | PSDK ecosystem expansion support. |
| Reported mission altitude | Maximum flight altitude reached during the mission: 8,861 m above sea level.May 2026 scientific mission departing Everest Base Camp, carrying an ozone measuring instrument and other equipment in thin, low-pressure air and complex wind conditions. |
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