A satellite in outer space has a gyroscope within it used for rotation and stabilization. The moment of inertia of the gyroscope is I, = 24.5 kg · m² about the axis of the gyroscope, and the moment of inertia of the rest of the satellite is I̟ = 5.00 x 105 kg · m² about the same axis. Initially both the satellite and gyroscope are not rotating. The gyroscope is then switched on and it nearly instantly starts rotating at an angular speed of 150 rad/s. How long (in s) should the gyroscope operate at this speed in order to change the satellite's orientation by 26.0°?

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A satellite in outer space has a gyroscope within it used for rotation and stabilization. The moment of inertia of the
gyroscope is I, = 24.5 kg · m? about the axis of the gyroscope, and the moment of inertia of the rest of the satellite is
1, = 5.00 x 105 kg · m? about the same axis. Initially both the satellite and gyroscope are not rotating. The gyroscope is
then switched on and it nearly instantly starts rotating at an angular speed of 150 rad/s. How long (in s) should the
gyroscope operate at this speed in order to change the satellite's orientation by 26.00?
Transcribed Image Text:A satellite in outer space has a gyroscope within it used for rotation and stabilization. The moment of inertia of the gyroscope is I, = 24.5 kg · m? about the axis of the gyroscope, and the moment of inertia of the rest of the satellite is 1, = 5.00 x 105 kg · m? about the same axis. Initially both the satellite and gyroscope are not rotating. The gyroscope is then switched on and it nearly instantly starts rotating at an angular speed of 150 rad/s. How long (in s) should the gyroscope operate at this speed in order to change the satellite's orientation by 26.00?
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