How would I create a script in MatLab to solve this. I must use the Bisection Method and there must be a nested function within.

8.39 The upward velocity of a rocket can be computed by the fol- lowing formula: mo -g where -upward velocity, the velocity at which fuel is ex- pelled relative to the rocket, mo = the initial mass of the rocket at time t-0,q the fuel consumption rate, and g the downward ac- celeration of gravity (assumed constant 9.81 m/s) Ifu 2200 ms, mo 160,000 kg, and q 2680 kg, compute the time at which v = 1000 m/s. (Hint: t is somewhere between 10 and 50 s.) Determine your result so that it is within 1% of the true value. Check your answer 8.39 The upward velocity of a rocket can be computed by the fol- lowing formula: mo -g where -upward velocity, the velocity at which fuel is ex- pelled relative to the rocket, mo = the initial mass of the rocket at time t-0,q the fuel consumption rate, and g the downward ac- celeration of gravity (assumed constant 9.81 m/s) Ifu 2200 ms, mo 160,000 kg, and q 2680 kg, compute the time at which v = 1000 m/s. (Hint: t is somewhere between 10 and 50 s.) Determine your result so that it is within 1% of the true value. Check your