The satellite's body C has a mass of 200 kg and a radius of gyration about the z axis of kz = 0.2 m. If the satellite rotates about the z axis with an angular velocity of 5 rev/s, when the solar panels A and B are in a position of θ = 0°, determine the angular velocity of the satellite when the solar panels are rotated to a position of θ = 90°. Consider each solar panel to be a thin plate having a mass of 30 kg. Neglect the mass of the rods.
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