Review Part A A medium-sized jet has a 3.8-m-diameter fuselage and a loaded mass of 85,000 kg. The drag on an airplane is primarily due to the cylindrical fuselage, and aerodynamic shaping gives it a drag coefficient of 0.37. How much thrust must the jet s engines provide to cruise at 260 m/s at an altitude where the air density is 1.1 kg/m3? Express your answer with the appropriate units. HA ? F = 111 KN Submit Previous Answers Request Answer X Incorrect; Try Again; One attempt remaining Provide Feedback Next >