Product overview
Doosan Mobility Innovation’s DP30M2S provides hydrogen fuel cell power for industrial UAVs, including infrastructure inspection and public safety monitoring missions. It is a separate-type power system with direct integration identified for the DS30W platform. Its modular construction allows customization of materials, stack design and system design for different aircraft. The U-shaped housing is intended to reduce flight drag, while the integrated internal structure helps protect internal components against damage from accidental drops during handling.
Integration planning must accommodate a 600 × 530 × 320 mm system weighing 6.9kg, with a separate listed weight of 12.7kg for the 10.8L hydrogen cylinder. Rated output is 2.7kW and peak output is 5kW. The battery-hybrid architecture lists two LiPo configurations and includes an emergency landing device. LTE and RF communications support the configuration, while DMI View provides system monitoring and configured flight functions. Operating temperature is limited to -5 to 40℃; storage temperature is -10 to 40℃.
Specifications
| Specification | Value & conditions |
|---|---|
| Product model | DP30M2S |
| Product type | Separate-type fuel cell system for UAVs |
| Platform integration | Directly fits the DS30W UAV platform |
| Dimensions (W × L × H) | 600(W) × 530(L) × 320(H) mm |
| Rated power | 2.7kW |
| Hydrogen pressure | 0 ~ 350bar |
| Peak power | 5kW |
| Operating temperature | -5 to 40℃ |
| System weight | 6.9kgFuel cell system. |
| Storage temperature | -10 to 40℃ |
| Hydrogen cylinder weight | 12.7kg10.8L hydrogen cylinder. |
| Battery configuration | LiPo (2,600mAh × 2)Hybrid battery option 1. |
| Battery configuration | LiPo (1,800mAh × 2)Hybrid battery option 2. |
| Communications | LTE, RF |
| Physical architecture | U-shaped design intended to reduce aerodynamic drag, with an integrated internal structure |
| Modular integration | Modular assembly with customization spanning fuel cell materials, stack design and system design |
| Hybrid power and emergency equipment | Battery-hybrid architecture supports transient power demand; an emergency landing device is fittedBattery-hybrid configuration. |
| System monitoring | Real-time monitoring of remaining hydrogen, voltage and currentUsing DMI View App. |
| Flight control functions | Flight control, automatic flight along configured routes and configurable return to the takeoff point when hydrogen is lowUsing DMI View App with the corresponding settings. |
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