Rocket propulsion equation: what's the error here?

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yucheng
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Equation for rocket motion:
$$\frac{d \mathbf{P}}{d t} = M\frac{d \mathbf{v}}{d t} - \mathbf{u}\frac{d M}{d t}$$

But $$\mathbf{F}=\frac{d \mathbf{P}}{d t}=M\frac{d \mathbf{v}}{d t}$$

So $$M\frac{d \mathbf{v}}{d t} = M\frac{d \mathbf{v}}{d t} - \mathbf{u}\frac{d M}{d t}$$

And $$- \mathbf{u}\frac{d M}{d t}=0$$

Now, what's wrong? Thanks in advance!
 
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Ok, I messed up. Momentum is conserved. So ##\mathbf{F}=0##!
 
yucheng said:
Ok, I messed up. Momentum is conserved. So ##\mathbf{F}=0##!
I am glad you sorted that out because it saved me some writing. More generally ##\vec F## represents the sum of external forces acting on the rocket. Also, you should be using total, not partial derivatives here.
 
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