Thrust is defined as the force produced by a propulsion unit, measured in Newtons, while thrust density refers to the thrust produced per unit area of the nozzle, measured in Newtons per square metre. Thrust density can indicate how effectively thrust is distributed over the nozzle area, with smaller nozzles potentially yielding higher thrust density for the same thrust. However, thrust density alone does not provide information about exhaust velocity or efficiency without additional data, such as the density of the exhaust stream. The discussion highlights that thrust density can be related to pressure but is not a direct measure of propulsion efficiency. Understanding these distinctions is crucial for evaluating different propulsion systems.