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Force produced by pushing against a reaction mass in space à la Newton's third law: "For every action there is an equal and opposite reaction." The thrust of a rocket engine is the forward force produced by expelling the exhaust mass (reaction mass) in the backwards direction.
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Can effective thrust in the more dense layers of the atmosphere be considered constant (as a...
It states the following:
The thrust load ratio is: $Psi = {T \over Mg}$
$T$ being the effective thrust, equal to the actual (constant) thrust minus the drag. … So the aerodynamic drag increases but the thrust remains the same hence the effective thrust changes. …