Right choice is (a) 2
For explanation I would say: Given, thrust per engine T = 10000 unit and thrust loading T.L. = 0.71
Now, take-off gross weight is 28000 units.
Now, number engines required is given by,
N = W*T.L. / T = 28000*0.71/10000 = 1.98.
We cannot use 1.98 engines so we will take the nearest integer. Hence, the answer will be 2.