Integration of Tsiolkovsky rocket equation

In summary, we discussed the use of the Tsiolkovsky rocket equation derivation to obtain the equation \Delta V = v_e \ln \frac {m_0} {m_1} by integrating the expression \frac{dV}{dt} = -\upsilon_e \frac{1}{m} \frac{dm}{dt} and using the fundamental theorem of calculus. We also mentioned the possibility of using a substitution to make the integration easier, and the concept of the derivative of ln(x) being 1/x, or ln|x| having a derivative of 1/x.
  • #1
LogicalTime
114
0
In the Tsiolkovsky rocket equation derivation there is a part that says:

[tex]\frac{dV}{dt} = -\upsilon_e \frac{1}{m} \frac{dm}{dt}[/tex]
"Assuming v_e, is constant, this may be integrated to yield:"

[tex]\Delta V\ = v_e \ln \frac {m_0} {m_1} [/tex]

How does this work? The differential is an operator and I am pretty sure you just can't cancel the dt. I wonder what assumptions are needed to be able to legally just remove the "dt"s though.

Thanks!
 
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  • #2
LogicalTime said:
In the Tsiolkovsky rocket equation derivation there is a part that says:

[tex]\frac{dV}{dt} = -\upsilon_e \frac{1}{m} \frac{dm}{dt}[/tex]
"Assuming v_e, is constant, this may be integrated to yield:"

[tex]\Delta V\ = v_e \ln \frac {m_0} {m_1} [/tex]

How does this work? The differential is an operator and I am pretty sure you just can't cancel the dt. I wonder what assumptions are needed to be able to legally just remove the "dt"s though.

Thanks!

Multiply both sides by dt, and then integrate both sides to get:

[tex]\int \frac{dV}{dt} dt = \int -\upsilon_e \frac{1}{m} \frac{dm}{dt} dt[/tex]

Now, the left side can be given the substitution u=V, du/dt= dV/dt or du = dV/dt dt. The right side can be given the substitution w=m, dw = dm/dt dt, thus turning your equation into...

[tex]\int du = \int -\upsilon_e \frac{1}{w} dw[/tex]

And both sides of those can obviously be integrated.
 
  • #3
Thank you for helping me to see the substitution. :-)
 
  • #4
You can also look at it this way:

[tex]\int_{t_0}^{t_f} dt~\frac{dV}{dt} = V(t_f) - V(t_0)[/tex]
by the fundamental theorem of calculus.

Similarly,

[tex]\int_{t_0}^{t_f}dt~\frac{1}{m}\frac{dm}{dt} = \int_{t_0}^{t_f}dt~\frac{d}{dt}\left(\ln m(t) \right) = \ln m(t_f) - \ln m(t_0) = \ln\left(\frac{m(t_f)}{m(t_0)}\right),[/tex]
again due to the fundamental theorem. We also recognized that [itex]d(\ln m(t))/dt = (1/m) dm/dt[/itex].
 
  • #5
Thanks! Another way to see it.

One further detail:
I think we have been leaving out the absolute value sign.
[tex] \int \frac{1}{w} dw = \ln |w| + c[/tex]

However wiki says this is true:

[tex] \frac{d}{dw} \ln(w) = \frac{1}{w} [/tex]

Assuming that is true then using the fundamental theorem of calc we would get an answer without the absolute value. I am not sure how to reconcile that. Do you guys understand this subtlety?
 
  • #6
We could have written the absolute value sign when we integrated, but m is presumably the mass, which is never negative, so we don't need it in this case. The absolute value sign appears in infinite integrals when it's not specified whether the variable is positive or negative, or in definite integrals when you know for sure the variable is negative (and don't feel like writing [itex]\ln (-x)[/itex] all the time).

If x is positive:

[tex]\frac{d}{dx}\ln x = \frac{1}{x}[/tex]

If x is negative, only ln(-x) makes sense, since the argument of the log must be positive. So:

[tex]\frac{d}{dx}\ln(-x) = \frac{1}{-x}(-1) = \frac{1}{x}[/tex]

Since the derivative of both ln(x) and ln(-x) gives 1/x, we can write this in compact form saying the derivative of ln|x| is 1/x.

(Note also that ln(ax) has a derivative of 1/x. So, if you differentiate ln(ax), to get it back when you integrate, you can write the arbitrary constant as ln(a), which gives back ln(ax)).
 
Last edited:
  • #7
Nice, that clears that up as well. Thank you!
 

What is the Tsiolkovsky rocket equation?

The Tsiolkovsky rocket equation is a mathematical formula that describes the motion of a rocket in terms of its mass, exhaust velocity, and the change in velocity it can achieve. It is named after Russian scientist Konstantin Tsiolkovsky, who first proposed it in 1903.

How is the Tsiolkovsky rocket equation used in rocket design?

The Tsiolkovsky rocket equation is used to calculate the amount of propellant needed for a rocket to reach a desired velocity. It is also used to determine the ideal ratio of fuel to payload for maximum efficiency.

What are the assumptions made in the Tsiolkovsky rocket equation?

The Tsiolkovsky rocket equation assumes that the rocket is traveling in a vacuum, there is no external force acting on the rocket, and the exhaust gases are expelled at a constant velocity.

How does the Tsiolkovsky rocket equation account for the changing mass of a rocket during flight?

The Tsiolkovsky rocket equation takes into account the changing mass of a rocket by using the concept of specific impulse, which is a measure of the efficiency of an engine. This accounts for the decrease in mass as fuel is burned during flight.

What are the limitations of the Tsiolkovsky rocket equation?

The Tsiolkovsky rocket equation does not account for the effects of gravity, air resistance, and other external forces. It also assumes that the rocket's engine is constantly firing at the same rate, which is not always the case in real-life situations.

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