Problem Diagram
Satellite in Deployed Position
Satellite in Stored Position


To accurately control the new satellite, small rocket thrusters will be used to rotate and move the satellite when in orbit. In order to know how long to fire the thrusters, the mass and moment of inertia must be known.
Due to the intricate shape of the satellite, you can't accurately calculate the moment of inertia. Your boss tells you to use the spin table to determine the moment of inertia experimentally.
What is known:
 The change in angular displacement Δθ is 4.459 rad.
 The change in angular velocity Δω is 1.784 rad/s
 The spin table generates a constant 100 N m torque during the length of the test.
 The time length of the test was not monitored.
