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The aircraft has a take-off speed of 310 km/h, a take-off weight of 16.5 t, and uses a 2 km take-off runway. Its cruising speed is 880 km/h and cruising altitude is 10 km.
a) Determine the aircraft's acceleration during take-off and the take-off time.
b) Determine the thrust of the engines during take-off.
c) Over what minimum distance does the aircraft reach cruising speed and altitude at that thrust F?

Your answer:

m/s2
s
N
m


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