I'm trying to understand the derivation of the Tsiolkovsky Rocket Equation
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$$\Delta v= \int_{t_0}^{t_1} \dfrac{|T|}{m_0 - t\Delta m}dt$$
The Wikipedia page confused me here :
where $T$ is thrust, $m_{0}$ is the initial (wet) mass and Δm is the initial mass minus the final (dry) mass
Which means that $$m_0 - t\Delta m = m_0 -t(m_0-m_{dry})$$
If the rocket launched at $t_0=0$ seconds and reaches the dry mass at $t_1 = 60$ seconds, then at $t_1$ we should expect an acceleration of $$a(t_1) =\dfrac{|T|}{m_{dry}}$$ but we get $$a(t_1) =\dfrac{|T|}{m_{0} - t_1 \Delta m} = \dfrac{|T|}{m_{0} - 60s \Delta m} $$
I am unsure if this is an error or not. I then derived the equation using a slightly different approach I made up which seemed more intuitive to me, instead of using $\Delta m$, I used the rate $r$ (kg/s) at which the fuel exits the system.
$$\Delta v= \int_{t_0}^{t_1} \dfrac{|T|}{m_f - tr}dt$$
Now if I we take the integral we obtain
$$\Delta v =-\dfrac{|T|}{r}\ln\left|\dfrac{m_0}{m_{dry}}\right|$$
My derivation seems wrong because I have a negative sign in front which doesn't make sense. Is there something that I missed?