New technical paper: Hybrid UAV Propulsion Systems for Longer Missions

Sky Power has released a new technical paper explaining how hybrid UAV propulsion systems can extend the performance limits of electric flight platforms. The paper shows how the combination of an internal combustion engine, generator, control electronics and electric propulsion can support longer flight times, greater range and higher payload capacity.

The paper is aimed at UAV manufacturers, system integrators and technical decision-makers working on long-endurance missions, VTOL applications, ISR platforms, BVLOS operations and sensor-intensive UAV systems.

What the technical paper covers

The paper provides a compact technical overview of serial hybrid UAV propulsion systems. It explains how an internal combustion engine drives a generator instead of the propeller directly. The generated electrical energy powers the UAV’s electric motors, avionics, communication systems, payload electronics and battery storage.

This approach allows the combustion engine to operate within an efficient RPM range, while the electric propulsion system manages power delivery during takeoff, cruise, transition or landing. The result is improved energy use, reduced load fluctuations and greater flexibility in UAV system design.

Key advantages for demanding UAV missions

Hybrid propulsion can be especially valuable for applications where battery capacity alone limits mission performance. Typical use cases include:

  • VTOL UAVs with high takeoff and transition power requirements
  • ISR and surveillance missions requiring long endurance
  • BVLOS operations over large distances
  • Sensor-intensive platforms with EO/IR, LiDAR, SAR or communication payloads
  • Infrastructure inspection, pipeline monitoring and maritime reconnaissance
  • Heavy-lift drones for logistics, medical supply or disaster relief

For these applications, a hybrid system can provide longer operating times, greater range and continuous electrical power for modern onboard systems.

Download the technical paper

Learn how hybrid UAV propulsion systems combine internal combustion engines and generators to extend endurance, increase payload flexibility and support the next generation of professional UAV applications.

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Fuel mixture preparation directly influences combustion stability, specific fuel consumption, load response, thermal stress and engine service life. For UAV manufacturers and system integrators, choosing the right fuel metering system is therefore an important part of propulsion system design and can affect efficiency, reliability and mission performance.

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Electronic fuel injection is particularly suitable for long-range UAVs, BVLOS missions, high-performance platforms, hybrid propulsion systems and applications with changing environmental conditions. EFI can improve fuel efficiency, combustion stability, altitude compensation, diagnostics and telemetry integration.

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A carburetor can be the right choice when a UAV platform requires maximum robustness, simple integration, low system complexity and predictable operating conditions. This makes carburetor-based engines especially relevant for applications where ease of maintenance, reliability and straightforward commissioning are more important than advanced digital engine control.

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A diaphragm carburetor meters fuel mechanically and does not require sensors, control units or electronic actuators. Electronic fuel injection, also known as EFI, uses sensor data and map-based control to adjust the fuel-air mixture more precisely across different operating conditions. For UAV manufacturers, the main difference lies in system complexity, control precision, integration effort and mission flexibility.

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