Cleonis
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PeterDonis said:The force measured by the thruster unit is equal to the momentum transferred by it to the ISS per unit proper time,
Naturally I agree that the propulsion from a thruster unit goes back to conservation of momentum: a rocket ejects small amounts of mass at extremely high velocity from its exhaust nozzle, resulting in acceleration of the rocket in the opposite direction.
We can attach that rocket to a larger object, such as ISS, to accelerate it. We can gage the force that is exerted upon ISS independently. For instance, we can use a force gage that works with a coiled spring. Or we can use properties of gas for force calibration. When the volume of a gas is halved its pressure doubles (to a first approximation, more accurate models are available). Bottom line: the way the force gage is calibrated is independent from the operation of the thruster unit.
Assume the thruster unit can vary the nozzle velocity of the exhaust (In other words, it can vary how hard the exhaust is accelerated.) We find that the force that is exerted is proportional to how hard the exhaust is accelerated. We find F=m*a
It's not clear to me how that proportionality could be seen as a matter of definition.
Cleonis