The mass flow rate through the nozzle of a rocket engine is 200 kg/s. the areas of the nozzle inlet and exit planes are 0.7 and 2.4 m2, respectively. on the nozzle inlet plane, the pressure and velocity are 1600 kpa and 150 m/s, respectively, whereas on the nozzle exit plane, the pressure and velocity are 80 kpa and 2300 m/s, respectively. find the thrust force acting on the nozzle.

1which body contains the majority of the mass in the solar system earth jupiter the moon the sun 2 what keeps the objects in the solar system such as planets orbiting around the sun the force of gravity the galaxy exerts on all objects within it including the solar system the great distance between the sun and the planets the sun's nuclear fusion which acts on each object the gravitational force between the sun and each object in the solar system