Which rotor turns in a plane perpendicular to the main rotor and is parallel to the fuselage's longitudinal axis, and is used to control torque and yaw?

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Multiple Choice

Which rotor turns in a plane perpendicular to the main rotor and is parallel to the fuselage's longitudinal axis, and is used to control torque and yaw?

Explanation:
The anti-torque rotor is the component that provides yaw control by counteracting the torque of the main rotor. In a typical single-rotor helicopter, the engine turns the main rotor, which would make the fuselage want to spin in the opposite direction. The anti-torque rotor, mounted at the tail, spins in a plane perpendicular to the main rotor’s plane (its disk is vertical) and its axis runs along the fuselage’s longitudinal axis. By varying the tail rotor thrust with the anti-torque pedals, you create a counter-torque that yaw-controls the aircraft and lets you steer. The pedal itself is just the control input to adjust this thrust, not the rotor that does the anti-torque work. An articulated rotor refers to a main rotor with hinges, not the anti-torque system, and an axis of rotation is a general term, not a rotor.

The anti-torque rotor is the component that provides yaw control by counteracting the torque of the main rotor. In a typical single-rotor helicopter, the engine turns the main rotor, which would make the fuselage want to spin in the opposite direction. The anti-torque rotor, mounted at the tail, spins in a plane perpendicular to the main rotor’s plane (its disk is vertical) and its axis runs along the fuselage’s longitudinal axis. By varying the tail rotor thrust with the anti-torque pedals, you create a counter-torque that yaw-controls the aircraft and lets you steer. The pedal itself is just the control input to adjust this thrust, not the rotor that does the anti-torque work. An articulated rotor refers to a main rotor with hinges, not the anti-torque system, and an axis of rotation is a general term, not a rotor.

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