Question 1 1 pts Calculate the fuel weight fraction required to climb from sea level to 25.0000 at maximum thrust under the fastest climb conditions for the following turbojet airplane. Assume the thrust specific fuel consumption is C.75/h. Wing Loading H2 lb/ft 2 /Wimax. 0.58 Cd0-0.013 K-0.019 Clmax-2.0 Mdr-3.88 NOTE: this is a very small number so, usu 4 digits after the decimal for your answer!!!!!