New Paper: Push or Pull Configuration in UAVs – Which Approach Delivers the Best Performance?

Understanding the Impact of Propeller Placement on Aerodynamics, Cooling, and Engine Integration

The choice between a push and pull propeller configuration is one of the most important design decisions in modern UAV development. It influences not only aerodynamic performance and flight efficiency, but also engine cooling, payload integration, vibration behavior, and the long-term reliability of the entire aircraft.

In its latest paper, Sky Power International explores the technical advantages and challenges of both propulsion concepts and examines how propeller placement affects thermal management, airflow, propulsion system integration, and mission effectiveness.

The paper provides valuable insights for UAV developers, system integrators, and aerospace engineers working on ISR platforms, long-endurance UAVs, tactical reconnaissance drones, and hybrid propulsion systems. It also highlights why modern UAV propulsion systems must be viewed as integrated systems where the engine, propeller, cooling concept, exhaust system, and airframe work together to achieve optimal performance.

Download the technical paper

Learn how push and pull propeller configurations affect aerodynamics, engine cooling, system integration and overall UAV performance.

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Propeller configuration affects cooling airflow, heat accumulation and engine temperature distribution. Sky Power considers thermal management, exhaust routing and vibration behavior as part of the complete UAV propulsion system.

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Pull configuration gives the propeller and engine cleaner airflow, which can improve efficiency and cooling. This supports stable operating conditions for Sky Power UAV engines in endurance-focused platforms.

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Push configuration is used in ISR UAVs because the front section remains clear for EO/IR cameras, radar or LiDAR systems. Sky Power engines support these platforms when propulsion, cooling and vibration behavior must be precisely integrated.

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In a pull configuration, the propeller is mounted at the front. In a push configuration, it is positioned at the rear, which keeps the UAV nose free for sensors but increases demands on cooling and engine integration.

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