What should be the value of thrust- to-weight ratio for a normal take-off so that the acceleration associated with the rate of climb is neglected?(a) 0.1(b) 0.2(c) 0.3(d) 0.4The question was posed to me during an interview for a job.This is a very interesting question from Climb and Descent Performance with Thrust-Producing Engines topic in portion Climb and Descent Performance of Aircraft Performance

What should be the value of thrust- to-weight ratio for a normal take-

1.	What should be the value of thrust- to-weight ratio for a normal take-off so that the acceleration associated with the rate of climb is neglected?(a) 0.1(b) 0.2(c) 0.3(d) 0.4The question was posed to me during an interview for a job.This is a very interesting question from Climb and Descent Performance with Thrust-Producing Engines topic in portion Climb and Descent Performance of Aircraft Performance
Answer» The correct choice is (c) 0.3 To explain I WOULD say: 0.3 MUST be the value of thrust- to-weight ratio for a normal take-off so that the acceleration ASSOCIATED with the rate of climb is neglected. This WAY the climb can be ASSUMED with constant airspeed and mach number.

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