Rocket moving through a cloud of dust, variable mass problem

In summary, the conversation discusses two methods for solving a problem involving the conservation of momentum and the application of Newton's second law. The first method involves the use of a variable-mass equation, while the second method applies the law over an infinitesimal time. Both methods lead to the same solution, but the use of the variable-mass equation is only necessary in cases where the mass is not constant. The conversation also clarifies that the mistake of treating mass as constant can lead to incorrect solutions.
  • #1
etotheipi
Homework Statement
The rocket, cross sectional area A and mass M, travels through a cloud of dust of density p. Determine the distance the rocket travels until its velocity is half of its initial velocity.
Relevant Equations
CLM
The first way to solve this is to just say, by conservation of momentum, that [itex]M_{0}v_{0}=(M_{0}+Apx)\frac{v_0}{2}[/itex] where [itex]Apx[/itex] is the mass of dust the rocket comes into contact with in a distance [itex]x[/itex].

For the second method, by considering the change of momentum of the dust in 1 second, we know the force applied to the rocket is [itex]-Apv^{2}[/itex]. So if we write down the Newton's second law relation, we get $$-Apv^{2} = (M_{0}+Apx) v \frac{dv}{dx}$$ which when solved does happen to give the same answer as in the first method. However, I thought Newton's second law is only applicable to closed systems of constant mass; so how is this equation giving the same answer?

Is it just a coincidence that method 2 works in this case, i.e. do we actually need to use the variable-mass equation of motion to do it properly?
 
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  • #2
etotheipi said:
Newton's second law is only applicable to closed systems of constant mass
You are only applying the law over an infinitesimal time, dt. During that time the rocket mass is effectively constant. Having obtained a valid equation you are then free to solve it.
 
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  • #3
haruspex said:
You are only applying the law over an infinitesimal time, dt. During that time the rocket mass is effectively constant. Having obtained a valid equation you are then free to solve it.

That's interesting. What's the difference between then just applying NII vs using the following variable mass equation, if it is even relevant at all?

Screenshot 2019-12-02 at 21.21.56.png
 
  • #4
etotheipi said:
That's interesting. What's the difference between then just applying NII vs using the following variable mass equation, if it is even relevant at all?

View attachment 253586
In the above equation, both terms on the left represent applied forces. In your equation in post #1, Fext is zero and the term on the left there is the other force in the equation above.
 
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  • #5
haruspex said:
In the above equation, both terms on the left represent applied forces. In your equation in post #1, Fext is zero and the term on the left there is the other force in the equation above.

Actually, this works nicely, thanks! I'm just a little confused as to when we then actually need to use the second equation instead of just using F=ma all of the time?
 
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  • #6
etotheipi said:
When I solve this I get a weird factor of ln(2)2ln⁡(2)2\frac{\ln{(2)}}{2} popping up.

Edit I think the mistake I made just now was writing the mass as just M, when it should instead be some function of t/x etc.?
Are you saying you treated M as constant in solving the equation? Yes, that would be wrong.

Your first equation in post #5 is often deduced from ##0=\frac{dp}{dt}=\frac{d(mv)}{dt}=m\dot v+v\dot m##. But this is invalid because in a closed system mass is constant. The only reason it works in problems such as in this thread is that the added mass had no momentum initially.
 
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FAQ: Rocket moving through a cloud of dust, variable mass problem

How does the variable mass of a rocket affect its movement through a cloud of dust?

The variable mass of a rocket, caused by the ejection of fuel and exhaust gases, can significantly affect its movement through a cloud of dust. As the mass decreases, the rocket experiences less resistance and therefore accelerates faster. However, as the mass decreases, the thrust also decreases, leading to a decrease in acceleration.

What is the significance of the dust cloud in this problem?

The dust cloud in this problem represents an external force acting on the rocket. As the rocket moves through the cloud, it experiences a force opposite to its direction of motion, which can affect its acceleration and trajectory.

How does the size of the dust particles affect the movement of the rocket?

The size of the dust particles can affect the resistance experienced by the rocket. Larger particles may cause more resistance, leading to a decrease in acceleration, while smaller particles may have less of an impact. However, the exact effect will depend on the density and composition of the particles.

How can we calculate the acceleration of the rocket in this problem?

The acceleration of the rocket can be calculated using Newton's Second Law of Motion, which states that the net force acting on an object is equal to its mass multiplied by its acceleration. In this problem, the net force is the difference between the thrust force and the resistance force caused by the dust cloud.

How does the rocket's velocity change as it moves through the dust cloud?

The rocket's velocity can change in several ways as it moves through the dust cloud. Initially, its velocity may decrease due to the increased resistance from the dust particles. However, as the rocket's mass decreases, the thrust force may also decrease, leading to a decrease in acceleration. Eventually, the rocket may reach a constant velocity as the thrust and resistance forces balance out.

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