How is Newton’s 3rd law applied in rocket propulsion

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I'm really wanting to get into physics more and I've had this question for a while. I do know a bit about rocketry as I think it's pretty cool but I'm still struggling to understand how Newton's 3rd law applies on a more microscopic level. In a rocket, propellant is used to produce often very hot gas going very fast. This gas then exits through a rocket nozzle. Newton's 3rd law says that this gas moving with a lot of force away from the rocket will cause the rocket to experience an equal and opposite force thus allowing the rocket to liftoff. I'm curious where the actual collisions happen as the rocket seems to just eject the exhaust without the particles "hitting" anywhere to allow the force to occur. If anything needs clarifying I'd be happy to try!

Best Answer

There are two ways to think about it, depending on how you want to think about gases. You can think of gasses as having a pressure. When a rocket is burning, there is a very high pressure inside the rocket. That pressure pushes gas downward, but also pushes up on the rocket.

The other approach is to think of individual molecules of gas. They aren't just going straight down. They bounce around with thermal energy (they're very hot). Those gas molecules sometimes collide with the rocket, imparting momentum to the rocket.

Both are valid ways of thinking about a rocket motor, it just depends on how you want to treat them. Sometimes its best to think of the gasses as a fluid. Other times its best to think of it as a bunch of particles. But both have a rationale for why the rocket goes upward.

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