9- Water flows steadily through a splitter as shown in Fig. with Q#10.08 m3/s, Q# 2 = 0.05 m3/s, D1 = D2 = 12 cm, D3 10 cm. If the pressure readings at the inlet and outlets of the splitter are P1 = 100 kPa, P2 = 90 kPa and P3 80 kPa, determine external force needed to hold the device fixed. Disregard the weight effects. 10- An orbiting satellite has a mass of 3400 kg and is traveling at a constant velocity of V0. To alter its orbit, an attached rocket discharges 100 kg of gases from the reaction of solid fuel at a speed of 3000 m/s relative to the satellite in a direction opposite V0. The fuel discharge rate is constant for 3s. Determine (a) the thrust exerted on the satellite, (b) the acceleration of the satellite during this 3-s period, and (c) the change of velocity of the satellite during this time period. Satellite msat Vo

9- Water flows steadily through a splitter as shown in Fig. with Q#10.08 m3/s, Q# 2 = 0.05 m3/s, D1 = D2 = 12 cm, D3 10 cm. If the pressure readings at the inlet and outlets of the splitter are P1 = 100 kPa, P2 = 90 kPa and P3 80 kPa, determine external force needed to hold the device fixed. Disregard the weight effects. 10- An orbiting satellite has a mass of 3400 kg and is traveling at a constant velocity of V0. To alter its orbit, an attached rocket discharges 100 kg of gases from the reaction of solid fuel at a speed of 3000 m/s relative to the satellite in a direction opposite V0. The fuel discharge rate is constant for 3s. Determine (a) the thrust exerted on the satellite, (b) the acceleration of the satellite during this 3-s period, and (c) the change of velocity of the satellite during this time period. Satellite msat Vo