The upward velocity of a rocket can be computed by the formula below. Compute for the time t at which the velocity is 1100m/s using Bisection method if u = 2200m/s, mo = 160,000Kg, q = 2680Kg/s and g = 9.8m/s². Tabulate the results. Use Ea≤ 0.0001 as terminating condition.
v = uLn [ m0/m0-qt ] - gt