For jet aircraft, thrust loading is greater than the climb gradient.

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Thrust-to-weight ratio (T/W) is a dimensionless ratio that indicates the performance of a vehicle propelled by a jet engine, propeller engine, or rocket. Wing loading (W/S) is the ratio of an aircraft's weight to its wing area.  Thrust-to-weight ratio is calculated by dividing the thrust of an airplane by its weight. Wing loading is calculated by dividing the mass of a plane or bird by the total area of its wings' upper surface.  Thrust-to-weight ratio is directly proportional to an aircraft's acceleration. An aircraft with a high thrust-to-weight ratio has high acceleration and excess... Show more

For jet aircraft, thrust loading is greater than the climb gradient.