Observe and Map
Thermal and visual information supports incident assessment. Sensor equipment, endurance and communications shape the aircraft requirements. [1]
YUNTU / PROPULSION ENGINEERING
Firefighting drones range from observation aircraft to platforms that carry suppressant or emergency equipment. This guide focuses on propulsion selection for developers of those aircraft: loaded mass, hover requirements and installation constraints.
Yuntu supplies propulsion units and integration support. We do not sell firefighting drones, extinguishing munitions or foam systems.

A firefighting drone is an uncrewed aircraft used in fire and emergency work. Some support observation and mapping; others are designed to carry suppressant or equipment. Propulsion requirements depend on the task, payload and operating conditions.
Thermal and visual information supports incident assessment. Sensor equipment, endurance and communications shape the aircraft requirements. [1]
Include suppressant, tanks and release equipment in the mass budget. Assess hover duration, changing payload and operating conditions.
Include hoses, tools or emergency supplies. Review suspended loads, attachment points and clearance with the airframe team.
Treat suppressant as part of the complete mass budget: include tanks, release gear, energy storage and the aircraft structure. Payload alone cannot determine a propulsion model.
Assess the loaded aircraft and the changing load during discharge. Check the intended hover duration, electrical and thermal limits, and the control requirements for relevant failure cases.
Use the cargo guide for thrust-margin arithmetic and the heavy-lift guide for suspended loads. These calculations are starting points for an engineering review.
Payload mass, access clearance, hover duration and local operating temperature.
Route distance, operating altitude, landing area and emergency equipment mass.
Hose or equipment load, building clearance, wind conditions and available operating space.
Package mass, attachment method, route and ground-team access.
| Design consideration | Ducted fan | Open rotor |
|---|---|---|
| Blade enclosure | Blades operate inside a duct. | Blade tips are exposed. |
| Installation footprint | Assess the complete duct, mounts and inlet clearance. | Assess rotor clearance and separation from nearby equipment. |
| Powered-lift integration | The duct can form part of the powered-lift installation. | Lift integration depends on the rotor and airframe layout. |
| Mission fit | Review inlet flow, thermal limits and installation loads. | Review rotor clearance, operating conditions and installation loads. |
This page does not claim ducted fans are more efficient than open propellers of the same diameter. Efficiency depends on disk loading, flight speed and installation.
| Model family | Maximum thrust | Product details |
|---|---|---|
| 60 | 60 kgf | View product 60 ↗ |
| 200 | 200 kgf | View product 200 ↗ |
| 500 | 550 kgf | View product 500 ↗ |
| 1000 | 1000 kgf | View product 1000 ↗ |
The 500 model currently provides 550 kgf maximum thrust. Model names identify the product family, not a continuous-hover rating. Confirm sustained thrust, duration, ambient conditions and installation limits with engineering.
A remaining-thrust calculation alone does not establish controllability or a safe landing after a failure.
Request a Propulsion ReviewA firefighting drone is an uncrewed aircraft used in fire and emergency work. Some observe and map an incident; others are designed to carry suppressant or equipment. Propulsion must be selected for the intended mission.
No. Fire-service drones can also provide visual or thermal information and support incident assessment. Payload-carrying platforms have different mass, installation and hover requirements.
Start from the complete loaded mass, including suppressant, tanks, release equipment and energy storage. Review the number of propulsion units, thrust margin, sustained hover and failure cases with the aircraft engineering team.
Ducted fans enclose the blades and offer powered-lift installation options. Review clearance around people, hoses and structures, as well as inlet flow and thermal conditions. Enclosed blades do not remove every operating hazard.
The outcome depends on the aircraft layout, control system and available thrust. Assess failure cases at aircraft level. Remaining thrust alone does not establish controllability or guarantee a safe landing.
No. Yuntu supplies electric ducted-fan propulsion units and supports aircraft developers with sizing and integration. We do not sell firefighting drones, extinguishing munitions or consumer camera drones.
No. We quote propulsion configurations. Share target MTOW, payload, lift-unit count, hover requirements and electrical supply for a propulsion review.
The missions can overlap. Firefighting drone describes an uncrewed aircraft by its task; eVTOL describes electric vertical take-off and landing capability. This page focuses on propulsion for uncrewed emergency platforms.
Share what you know. Payload and airframe details can be refined during the engineering review.
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