Any ship that would fly or glide requires Lift and Drag IS an issue.
It's called the "Lift to Drag" Coefficient.
The lift to drag ratio (L/D) is the amount of lift generated by a wing or airfoil compared to its drag. The lift/drag ratio is used to express the relation between lift and drag and is determined by dividing the lift coefficient by the drag coefficient, CL/CD. A ratio of L/D indicates airfoil efficiency.
I know it's hard to grasp.
I am 42, have been flying since 17 years old. I'll ask again, why would any of our ships require aerodynamic lift , when they are capable of producing more than enough thrust to overcome gravity and drag.
These ships would only need a lifting body due to an engine out situation, one slight problem though, no elevators, ailerons or rudder. Without thrusters, that lifting body is basically an uncontrolled glide into the dirt.
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