Rocket propulsion equation: what's the error here?

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SUMMARY

The discussion centers on the rocket propulsion equation and the misapplication of momentum conservation principles. The equation presented is $$\frac{d \mathbf{P}}{d t} = M\frac{d \mathbf{v}}{d t} - \mathbf{u}\frac{d M}{d t}$$, which leads to confusion regarding the forces acting on the rocket. The key error identified is the incorrect use of partial derivatives instead of total derivatives, which is crucial for accurately representing the dynamics of rocket motion. Ultimately, the conclusion is that when momentum is conserved, the net external force $$\mathbf{F}$$ acting on the rocket equals zero.

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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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