Thanks Show that under unpowered flight conditions where lift, drag, and weight

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Show that under unpowered flight conditions where lift, drag, and weight forces are in equilibreum, that the glide slope, theta (i.e., the angle between a plane's fuselage and the horizontal direction) is given by tan theta = Cq/CL . Here, CD and CL are the lift and drag coefficients, respectively. For the space shuttle returning to earth, assume that C L is 10 times larger than Cd and assume that the atmosphere effectively begins a t an altitude of 60 miles. How far can the shuttle glide, unpowered, before landing?

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