Lift/Drag ratio of the wing...
You build an aeroplane that weighs X designed to carry Y people etc. Physics shows that Lift has to equal Weight. The ratio of Lift to Drag is defined by the characteristics of the wing...say 10:1...also gives approx glide ratio. Thrust only ever needs to be "a bit more than" drag (over simplification) so those two forces will only ever "need" to be a small proportion of the Lift and Weight.
By the way, there are FIVE forces...CASA.