Overview

Every gram removed affects flight time and payload, but low mass alone is not enough — stiffness and vibration behavior have to hold too.

We support UAV programs through propellers, interface parts, covers, panels, and structural body components that must work in real platform conditions.

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UAV & Aerospace

Balancing weight reduction with structural behavior

In aviation applications, reducing weight delivers a direct performance advantage; but a structure that is too compliant can negatively affect overall system behavior. Fiber orientation, local stiffness, connection areas, and vibration behavior are therefore evaluated not against a weight target alone, but together with the part's role within the platform.

UAV & Aerospace

Components developed around the mission profile

Even within the same aircraft family, priorities such as takeoff, cruise, payload, flight endurance, or low noise can call for different design decisions. For propellers and structural composite components, we base geometry and material selection on the real mission profile, not just the nominal operating point.

Overview

We support UAV programs through propellers, interface parts, covers, panels, and structural body components that must work in real platform conditions.

Composite Propellers

Every gram removed affects flight time and payload, but low mass alone is not enough — stiffness and vibration behavior have to hold too.

Flight certification, airworthiness approval, and platform-level flight-test results remain the program's and the customer's responsibility; Tulkas does not claim flight-test outcomes, airworthiness class, or certification status for any part.

Composite Manufacturing
Highlights

Highlights

Every gram removed affects flight time and payload, but low mass alone is not enough — stiffness and vibration behavior have to hold too Motor and propeller interface points carry concentrated load and vibration, so tolerance consistency there matters more than on the rest of the airframe

Approach

Approach

We support UAV programs through propellers, interface parts, covers, panels, and structural body components that must work in real platform conditions.

Questions?

Here are some answers.

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Yes. The engineering approach adapts to the platform's load case and mission profile rather than assuming one airframe type.

Yes. Geometry can be developed from a defined function and load case; a finished CAD model is not a prerequisite to start.