An airplane with two jet engines has the following properties: Wing Area, S = 50 m Aspect Ratio, AR = 6.5 Oswald Efficiency Factor, e = 0.87 Parasite Drag Coefficient, CD. = 0.03 Lift Coefficient, C = 0.11(a+3) where a is the angle of attack in degrees Stall angle of attack, astall 12 Maximum thrust of each jet engine, TA= 500B+40000 N at standard sea level Friction coefficient between the runway and the tires, = 0.1 This aircraft requires a lift-off distance of 10A+250 m at standard sea level. Using this information, determine the rate of climb at standard seal level if the angle of attack is 3 degrees. (50 pts) Note: A is the 10th digit in your student ID number while B is the 11th. SLO 1.44 W 8PSCL.max (T-[D+u, (W-L)]av}