A 2000 kg rocket is launched upwards. Its mass decreases at 11 kg/s until the mass is 50kg (empty shell ). While the fuel is still burning, the rock is propelled upwards with a force of 27, 500N. there is air drag, FD = - C*v^2, where C depends on the rocket's height because the air gets thinner as the rocket goes up. C = 10*e^(-h/3000) How high does the rocket get before running out of fuel

A 2000 kg rocket is launched upwards. Its mass decreases at 11 kg/s until the mass is 50kg (empty shell ). While the fuel is still burning, the rock is propelled upwards with a force of 27, 500N. there is air drag, FD = - Cv^2, where C depends on the rocket's height because the air gets thinner as the rocket goes up. C = 10e^(-h/3000) How high does the rocket get before running out of fuel