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The thrust required during the take-off is a function of ________

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The thrust required during the take-off is a function of ________

(a) time

(b) fuel

(c) weight

(d) lift

I have been asked this question in an international level competition.

This is a very interesting question from Climb Rate in division Climb and Descent Performance of Aircraft Performance

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Right option is (c) weight

Easiest explanation: The thrust required during the take-off is a function of weight, altitude and temperature i.e. WAT. Thrust is directly proportional to airspeed. This means the thrust increases with increase in airspeed and decrease with decrease in decrease in airspeed. The airspeed best for rate of climb to close to that of their minimum drag speed.

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