why is this wrong...THRUST?? i showed work! 1. The problem statement, all variables and given/known data A rocket for use in deep space is to have the capability of boosting a total load (payload plus the rocket frame and engine) of 2.25 metric tons to a speed of 10 000 m/s. If a different fuel and engine design could give an exhaust speed of 4600 m/s, what amount of fuel and oxidizer would be required for the same task? metric tons 2. Relevant equations vf=ve ln(mi/mf) 3. The attempt at a solution 10000=4600ln(x/2.25) x= 19.71 but its wrong. can you help?