5.30 The fighter Super Etendard has a takeoff mass of 12,000 kg, a wing area of 28.4 m, and a jet engine with 49 KN of thrust. Assume it has 5,000 kg of fuel and the following data: AR = 3.23, e = 0.78, CD, = 0.024, C= 0.9 lb/h/lb, CLmax = 1.8 If cruising at 35000 ft; determine a. Maximum range b. Maximum endurance