Select an aircraft of your choice and answer the following 

 

 

Show all work, Highlight your Answers, and use English units Select and identify your aircraft: :: PC12/47. Research and provide the following data for your selected aircraft (search the internet): A. Maximum Takeoff, Weight (MTOW) [lbs]: 10,450 16 B. Engine Type and Rated Thrust [lbs]: PT6A-67B C. Total Available Thrust (sum of all engines for multiengine aircraft) [lbs]: 1200 D. Maximum Rate of Climb [ft/min]: 1,9.20 E. Take-off distance at MTOW [ft]: 2,600 Uniformly Accelerated Rectilinear Motion and Newton's Law of Momentum Equations: F = ma A=F/M fps^2 KE = 12 mV m = W/g slugs g=32.2 ft/sec Takeoff distance (s) = VF2 12a ft PE = Wh HP= TV kts/325 1 kt = 1.69 ft/sec Remember to keep track of units, convert as required, and express answers in English units. Next complete the following: 1. Find the mass of your aircraft, using A & C from above. (m = W/g) 2. Find the Acceleration of your aircraft using the total thrust you found. (A=F/Mass. Note in this case F=Force of Total Thrust of your engines in C above and m from #1.) 3. If your aircraft lifted off the ground at 150kts, what would be the length of the takeoff run (in feet)? (Takeoff distance (s) = VF2 /2a. Watch for unit conversions, use a from #2.)