Product overview
The Doosan DS30W combines a DMI hydrogen fuel-cell power pack with a lightweight, eight-axis airframe for industrial flight operations. Folding arms simplify handling and setup, while carbon-fiber landing gear reduces weight and absorbs external impacts during emergency landings. The aircraft measures 1,850 × 1,850 × 815 mm excluding propellers and has a 1,990 mm wheelbase. System weight depends on the hydrogen cylinder configuration: 21.9 kg with the 10.8 L tank or 20.9 kg with the 7 L tank. Rated power is 2.7 kW.
The DS30W accommodates different payload pods, with customized UAV solutions offered for customer requirements. An installed 4G/LTE module enables real-time monitoring and transmission of hydrogen fuel-cell data, while Doosan’s ground control station supports flight-route planning. Maximum payload is 3 kg and maximum takeoff weight is 24.9 kg. Endurance is 120 minutes without payload, and maximum flight operating distance is up to 80 km. Wind resistance is 12 m/s, with an operating temperature range of -5 to 40 °C. Protective packaging supports transport in an ordinary SUV, van or pickup.
Specifications
| Specification | Value & conditions |
|---|---|
| Model | DS30W |
| Dimensions (W × L × H) | 1,850 × 1,850 × 815 mmExcluding propellers. |
| Rated power | 2.7 kW |
| Wheelbase | 1,990 mm |
| System weight with larger tank | 21.9 kgWith 10.8 L tank. |
| System weight with smaller tank | 20.9 kgWith 7 L tank. |
| Maximum takeoff weight | 24.9 kg |
| Endurance | 120 minWithout payload. |
| Maximum payload | 3 kg |
| Hydrogen cylinder capacity | 10.8 / 7 L |
| Wind resistance | 12 m/s |
| Operating temperature | -5 to 40 °C |
| Maximum flight operating distance | Up to 80 km |
| Product configuration | Hydrogen fuel-cell UAV flight platformEquipped with a DMI fuel-cell power pack. |
| Airframe architecture | Eight-axis structure |
| Arm construction | Folding arms |
| Landing gear material | Carbon fiber |
| Monitoring communications | 4G/LTE module for real-time monitoring and transmission of hydrogen fuel-cell dataInstalled onboard. |
| Mission planning | Flight route planningUsing the Doosan-provided ground control station. |
| Payload integration | Supports different payload pods, with customized UAV solutions offered for customer requirements |
| Ground transport | Transport in an ordinary SUV, van or pickupWith protective packaging whose internal structure matches the landing gear. |
| Landing gear impact absorption | Carbon-fiber landing gear reduces airframe weight and absorbs external impacts during emergency landings.During emergency landings. |
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