A reaction wheel is a flywheel mounted on a spacecraft that can be spun up or down to produce a controllable torque about the spacecraftβs axes without expending propellant. By conserving angular momentum, the wheelβs change in spin angular momentum is transferred to the spacecraft, allowing precise attitude adjustments.
The torque generated by a reaction wheel is directly related to its moment of inertia (Iw) and the angular acceleration (alpha) applied to the wheel. The fundamental relationship is:
I_{w} = wheel moment of inertia (kgΒ·mΒ²)
alpha = wheel angular acceleration (rad/sΒ²)
To size a reaction wheel, engineers first define the required steadyβstate torque for the mission, then select a safety factor to account for uncertainties. The required wheel inertia is calculated by rearranging the torque equation, and the wheelβs physical dimensions and mass are chosen to meet this inertia while staying within speed and mass constraints.
How does a reaction wheel work in a spacecraft?
What is the relationship between moment of inertia and angular acceleration for a reaction wheel?
Why are reaction wheels important in spacecraft?
What factors affect the sizing of a reaction wheel?
Can reaction wheels be used indefinitely in a spacecraft?
How do you calculate the moment of inertia for a reaction wheel?
What are the advantages of using reaction wheels over thrusters for attitude control?
Results are for informational purposes only and do not constitute professional advice.
