martillo Posted November 28 Posted November 28 (edited) The problem in the rocket's equation is not in its derivation but in the final result. The force on the rocket is finally found to be F = mdv/dt = -vedm/dt and as dv/dt = a the force is F = ma and not dp/dt. Edited November 28 by martillo
Mordred Posted November 28 Posted November 28 (edited) Might help if you look at the time aspect imsteas of writing \[a=\frac{dv}{dt}\] Write \[a(t)=\frac{dv}{dt}\] Secondly momentum includes mass via \[p=m*v\] So where is the issue ? Others have tried explaining this to you in the older thread Edited November 28 by Mordred
martillo Posted November 28 Author Posted November 28 I don't understand your point. p = mv and dp/dt = mdv/dt + vdm/dt what is different from mdv/dt = ma for variable mass systems like the rocket. The force on the rocket is found to be F =ma what is not dp/dt.
swansont Posted November 28 Posted November 28 ! Moderator Note You had a thread on this already. It was locked. Don’t be hijacking someone else’s thread to bring it up
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