Prior to deployment of its two instrument arms AB, the spacecraft shown in the upper vie...

Prior to deployment of its two instrument arms AB, the spacecraft shown in the upper view is spinning at the constant rate of 1 revolution per second. Each instrument arm, shown in the lower view, has a mass of 10 kg with mass center at G. Calculate the tension T in the deployment cable prior to release. Also find the magnitude of the force on the pin at A. Neglect any acceleration of the center O of the spacecraft.