C++ programming

hen they ks A small rocket with an initial weight of 3000 lb, including 2400 lb of fuel, is fired vertically upward. The rocket burns fuel at the rate of 40 Ib/sec, which develops a thrust of, T. of 7000 lb. Considering that the drag force is proportional to the square of the velocity, v, the differential equation of motion from Newton's second law is found to be s been h the thei Ab OR dv K dt m mt Where 3000-40t 0 ts60 0