! Required information The Lockheed Martin F-16 is in a vertical accelerated climb. Some characteristics of this airplane from Jane's All the World Aircraft are: wing area = 27.87 m, typical combat weight = 8,273 kgf, sea level static thrust from the single GE F110 jet engine = 131.6 kN. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. L W Horizontal Flight path Voo R/C = Voo sin 0 Assume the subsonic value of the zero-drag coefficient is 0.016 and the transonic value of the zero-lift drag coefficient at Mach 1 is 2.3 times its subsonic value, a typical increase that occurs in the drag-divergence transonic flight region. Calculate the value of the summation of forces in the direction of the flight path. The value of the summation of forces in the direction of the flight path is 1.5 x 105 N.