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?

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.	0.4
Answer» D. 0.4