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In water rockets, I found this equation: h= (Mi/Mr) * (Mi/Mr) * (Pi/density of water*g). How did I get this equation?
I have a question about water rockets. I found this equation: h= (Mi/Mr) * (Mi/Mr) * (Pi/density of water*g). How did I get this equation?
This equation is called the rocket altitude equation, and it can be derived from the energy conservation principal. It relates the height achieved by a water rocket to the initial mass, the final mass, and the density of water. Would you like me to explain it in more detail?