Question

thrust available during takeoff: 3000lb turbojet engine combined average drag and rolling friction: 500lb gross weight:10,000lb takeoff speed 120 knots sea level strandard conditions. 1) calculate the airplanes acceleration 2) what should the airspeed be at the 1000 ft runway marker? 3) calculate the no-wind takeoff distance 4)if the weight is increased to 15,000 lb airplane if there is a 12 knot headwind 5) calculate the no-wind takeoff distance for the 10,000 lb airplane operating from an airfield where the density ratio is 0.8

Answer 1