Problem 2: The 300 metric tonne jet airliner has four engines, each of which produces a nearly constant thrust of 180 kN during the takeoff roll. Determine the length s of runway required if the takeoff speed is 220 km/hr. Compute s first for an uphill takeoff direction from A to B and second for a downhill takeoff from B to A on the slightly inclined runway. Neglect air and rolling resistance. Ans. (a) S-807 m (b) s#751 m

University Physics Volume 1
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Chapter6: Applications Of Newton's Laws
Section: Chapter Questions
Problem 33P: A large rocket has a mass of 2.00106kgat takeoff, and its engines produce a thrust of 3.50107N . (a)...
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Problem 2: The 300 metric tonne jet airliner has four
engines, each of which produces a nearly constant thrust of
180 kN during the takeoff roll. Determine the length s of
runway required if the takeoff speed is 220 km/hr.
Compute s first for an uphill takeoff direction from A to B
and second for a downhill takeoff from B to A on the
0.5°
Horizontal
slightly inclined runway. Neglect air and rolling resistance.
Ans. (a) S-807 m (b) sF751 m
Transcribed Image Text:Problem 2: The 300 metric tonne jet airliner has four engines, each of which produces a nearly constant thrust of 180 kN during the takeoff roll. Determine the length s of runway required if the takeoff speed is 220 km/hr. Compute s first for an uphill takeoff direction from A to B and second for a downhill takeoff from B to A on the 0.5° Horizontal slightly inclined runway. Neglect air and rolling resistance. Ans. (a) S-807 m (b) sF751 m
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