The 200-kg satellite has a radius of gyration about the centroidal z axis of k_z = 1.25 m. Initially it is rotating with a constant angular velocity of ω₀ = {1500 k} rev/min. If the two jets A and B, both in the x–y plane, are fired simultaneously and produce a thrust of T = (5e ^-t/10) kN, where t is in seconds, determine the angular velocity of the satellite, five seconds after firing.

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T = (5e-1/10)) KN 1.5 m x N B 1.5 m y T = (5e-1/10)) kN