1 point. Determine the Dynamic Pressure in psf, a, on the X15 if the Coefficlent of Lift 1 and and the wing loading is 170 psf at touchdown given the following reported conditions (use only if needed): X15 is at manimum weipht, X15 surface wing area 5200ft2 Edwards lakebed density altitude is 2,303 feet above mean sea level (M5L), Temperature is 11 degrees Centigrade, Winds are calm and variable. density tho at 2.303 feet MSL is (0.9344)[0.002377]=0.002221 slugs (ft3. Type vour answer- 1 proint The landing indicated airspeed of the X15 at maximum weight is 224 knots (true airspeed - 232 linots)and that is too fast even for landing on the lakebed at Edwards. If the 15 must land no faster than 135 knots indicated airspeed when the CL=1.0. What value in pounds must its weight not exceed at landing 2 (Note if needed: wing area S = 200tt2)(1knot1.688fosit Type your answer- Ipolit When the X15 lands at a safe wing loading of 61.7 pst with an indicated airspeed of 135 knots, the landing Coethcient of tift = 1.0. What is the one "Fre" epulvalent stail airspeed in knots when C12=1,3 or A OA stal=15 degrees? 1 point. Determine the Dynamic Pressure in psf, a, on the X15 if the Coefficlent of Lift 1 and and the wing loading is 170 psf at touchdown given the following reported conditions (use only if needed): X15 is at manimum weipht, X15 surface wing area 5200ft2 Edwards lakebed density altitude is 2,303 feet above mean sea level (M5L), Temperature is 11 degrees Centigrade, Winds are calm and variable. density tho at 2.303 feet MSL is (0.9344)[0.002377]=0.002221 slugs (ft3. Type vour answer- 1 proint The landing indicated airspeed of the X15 at maximum weight is 224 knots (true airspeed - 232 linots)and that is too fast even for landing on the lakebed at Edwards. If the 15 must land no faster than 135 knots indicated airspeed when the CL=1.0. What value in pounds must its weight not exceed at landing 2 (Note if needed: wing area S = 200tt2)(1knot1.688fosit Type your answer- Ipolit When the X15 lands at a safe wing loading of 61.7 pst with an indicated airspeed of 135 knots, the landing Coethcient of tift = 1.0. What is the one "Fre" epulvalent stail airspeed in knots when C12=1,3 or A OA stal=15 degrees