DrStupid said:
Is this just your personal opinion or can you proof it?
For systems of constant mass, the equation
$$
\mathbf F_{ext}=\frac{d\mathbf p}{dt}
$$
with ##\mathbf p =m\mathbf v## is generally valid because it is equivalent to ##\mathbf F_{ext}=m\mathbf a##, which we know is valid for such systems.
For systems of variable mass, the equation
$$
\mathbf F_{ext}=\frac{d\mathbf p}{dt}
$$
with ##\mathbf p =m\mathbf v## is generally invalid. Why? First, it does not take into account direction in which the leaving parts move. But this is important for the resulting motion. Also, this equation can be rewritten into form
$$
\mathbf F_{ext} = \frac{dm}{dt}\mathbf v + m\frac{d\mathbf v }{dt}
$$
which shows it is inconsistent with the Galilei relativity principle: the term ## \frac{dm}{dt}\mathbf v## depends on the frame of reference but the other terms do not. Furthermore, this equation leads to motion inconsistent with the law of conservation of momentum of isolated system. This law leads to the correct equation of motion
$$
\mathbf F_{ext} + \mathbf F_{exh} = m\frac{d\mathbf v}{dt}
$$
where ##\mathbf F_{ext}## is the force due to external bodies and ##\mathbf F_{exh} ## is the force due to leaving parts (exhaust gases in the case of a rocket).