Product overview
The Doosan Mobility Innovation DT30X is an integrated hydrogen fuel cell flight platform for industrial missions, including long-distance inspection and large-area surveying. Its DM30 power pack supplies the aircraft, with the fuel cells housed internally to reduce their susceptibility to water. The aircraft measures 1,600 × 1,600 × 675 mm and has a 1,600 mm wheelbase. Its maximum payload is 5 kg; the specified 150-minute flight time applies with no payload, making that qualification important when planning an equipped mission.
An integrated ground control system supports flight-path planning, while a cloud platform downloaded through a plugin enables mission management from different devices. Standard communication range is 10 km, with an optional 10–50 km configuration. Aircraft weight depends on the hydrogen cylinder: 20 kg with a 12 L Type 3 cylinder or 21 kg with a 10.8 L Type 4 cylinder. Maximum takeoff weight is 24.9 kg. The transport package measures 980 × 790 × 570 mm and is intended for carriage in an SUV.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer | Doosan Mobility Innovation |
| Model | DT30X |
| Product configuration | Fully integrated hydrogen fuel cell drone with a fuel cell power pack |
| Intended applications | Long-distance inspection and large-area surveying |
| Fuel cell placement | Fuel cells housed inside the drone to reduce susceptibility to water |
| Power pack | DM30 power pack with software and hardware for stable power delivery |
| Ground control | Integrated GCS system for flight-path planning |
| Mission management | IoT cloud platform supports flight-mission management from different devicesCloud platform downloaded via plugin. |
| Package dimensions | 980 × 790 × 570 mm (L × W × H) |
| Maximum payload | 5 kg |
| Dimensions | 1,600 × 1,600 × 675 mm (W × L × H) |
| Release date | 2023.12 |
| Maximum flight speed | 18 m/s |
| Wheelbase | 1,600 mm |
| Maximum ascent speed | 4 m/s |
| Weight | 20 kg with 12 L Type 3 cylinder; 21 kg with 10.8 L Type 4 cylinder20 kg with 12 L Type 3 cylinder; 21 kg with 10.8 L Type 4 cylinder. |
| Maximum descent speed | 2 m/s |
| System weight | 10 kg with 12 L Type 3 cylinder; 11 kg with 10.8 L Type 4 cylinder10 kg with 12 L Type 3 cylinder; 11 kg with 10.8 L Type 4 cylinder. |
| Communication range | 10 km standard; 10–50 km optional10 km standard configuration; 10–50 km optional configuration. |
| Maximum takeoff weight | 24.9 kg |
| Maximum altitude | 3,500 m |
| Flight time | 150 minNo payload. |
| Wind resistance | 10.8–13.8 m/s |
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