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Flight control systems Primary Flight Electromechanical Actuation for UAV’s Saab's primary actuator system is developed as a modular system with adaptation of a wide range of existing components. The system is ...
Torque: 1.07 Nm - 11.43 Nm
Design Features Slotless, brushless stator design provides zero cogging torque for unsurpassed velocity control Smoother velocity than with standard DC brush-type motors with the advantage of reliable brushless technology Standard NEMA ...
AEROTECH
Torque: 0.03 Nm - 0.14 Nm
Design Features Standard NEMA frame sizes Rare-earth magnets maximize performance Skewed stator design minimizes torque ripple and cogging for smooth velocity control over a wide speed range Optional IP65-level construction allows ...
AEROTECH
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