2) Satellite payloads are hurled into space by a carbon fiber tether in SpinLaunch's vacuum chamber. The tether has a length L = 30 m, width W = 3 m, and a mass MT = 6300 kg. The satellite payload can be considered a cylinder with a length LS = 3 m, radius R = 0.6 m and mass MS = 200 kg. Calculate the moment inertia of the tether and satellite payload system about an axis through the center of mass of the tether.