mo The Tsiolkovsky rocket equation is Au = v. In It calculates the maximum possible change in velocity for a rocket based on several parameters. v. is the velocity of the rocket's exhaust gasses (the fire part). mo is the initial mass of the rocket, including its fuel. my is the final mass of the rocket once all its fuel has been used. Calculate the maximum possible velocity change for a rocket if its exhaust gasses travel m 2500-, its initial mass is 25000/g, and its final mass is 1900/g. Round your answer to the nearest integer. m Au m For reference, a rocket needs Av of about 9400- in order to acheive orbit around the Earth