How does a sudden doubling of the mass of a star affect the orbit of a planet?

In summary, the mass of the star doubles, and the orbiting planet experiences a new E of -3/2U. The kinetic energy stays the same, but the orbit becomes less circular.
  • #1
marmot
55
1
Suppose you have a star of mass M and a planet of mass m orbiting around it. The orbit is circular. m<<<M. U of course is -GmM/r^2.

E of course is going to be -U/2 and kinetic energy U/2 due to the virial theorem.

What would happen if the mass of the star suddenly doubles?



This is a practice test question. Now, if it doubles, the kinetic energy is going to stay the same because the angular momentum won't suffer a torque (because force is radial). However U will double.

So we are going to have a new E of -3/2U where U=-GmM/r^2.

Now this seems clear to me however. The test then asks the for the kind of orbit the planet is going to experience. The question does not make sense because if it was circular before, and now E is more negative, then the eccentricity will be an imaginary number so it would not be physically possible.

Now, I did a similar homework problem to this but the star instead halves. If the star halves and the orbit was originally circular, E is going to be 0 so the orbit will be a parabola and unbound. However, here I am experiencing instead that the star doubles, so E is going to be more negative than before. What am I supposed to answer here?
 
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  • #2
Hi, marmot. Your dimensions don't match. The formula you provide for energy doesn't have units of energy. So you need to do some rethinking.
 
  • #3
marmot said:
Now, if it doubles, the kinetic energy is going to stay the same because the angular momentum won't suffer a torque (because force is radial).
That's not quite right. You have a non-physical situation here (masses don't just suddenly double, after all). You have to make some physically real assumptions, and conservation of linear (and angular) momentum being key. In other words, you are implicitly assuming momentum is conserved. Make that assumption explicit and be done with it.

Another way to look at this: To get an instantaneous change in velocity you need an impulsive force. Are there any impulsive forces involved here? (The answer is no.)

So we are going to have a new E of -3/2U where U=-GmM/r^2.
That is not correct. Look at the units. What is the equation for potential energy?

Now this seems clear to me however. The test then asks the for the kind of orbit the planet is going to experience. The question does not make sense because if it was circular before, and now E is more negative, then the eccentricity will be an imaginary number so it would not be physically possible.
What is the new Vmin, the minimum possible energy? The reason that orbital energy cannot be less than Vmin is because that would require an imaginary speed. The speed hasn't changed: It is still a real number.
 
  • #4
oh geez. sorry! i know that U=- GmM/r, i poisted force not energy! sorry i am sleepy right now.
 
  • #5
First the practice test is:

http://www.pa.msu.edu/courses/2009spring/PHY321/handouts/PHY321-PracticeMT3-09.pdf

I am referring to the last part of the first page.

D H said:
That's not quite right. You have a non-physical situation here (masses don't just suddenly double, after all). You have to make some physically real assumptions, and conservation of linear (and angular) momentum being key. In other words, you are implicitly assuming momentum is conserved. Make that assumption explicit and be done with it.

Isnt that what I am doing though? t=rxF, so if the force is parallel to the lever there is no torque and what changes angular momentum is torque. So if that force field changes, i.e. mass increases, it would not affect the momentum because it exerts no torque.

Another way to look at this: To get an instantaneous change in velocity you need an impulsive force. Are there any impulsive forces involved here? (The answer is no.)


That is not correct. Look at the units. What is the equation for potential energy?

yeah i know


What is the new Vmin, the minimum possible energy? The reason that orbital energy cannot be less than Vmin is because that would require an imaginary speed. The speed hasn't changed: It is still a real number.[/QUOTE]

So is the orbit still circular? I was referring to this when I said imaginary:

http://img15.imageshack.us/img15/7063/eccentricity.png

If the eccentricity is already zero for the circle, and the only thing that changes in this equation is E (which becomes more negative) then the square root will give imaginary.

EDIT: Actually, nevermind. myu also changes. But still, I had the impression that for a certain angular momentum, the more negative the energy the more circular the orbit, and in this case wouldn't the orbit be more negative than circular itself?
 
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  • #6
marmot said:
Isnt that what I am doing though?
No, it isn't. Torque is not needed and does not answer the question. For example, invoking torque as an explanation does not explain why the radial component of velocity doesn't instantaneously change.

So is the orbit still circular?
What is the new circular orbital velocity at the given radial distance? Is the planet's velocity vector equal to this? If not, the orbit cannot be circular.

But still, I had the impression that for a certain angular momentum, the more negative the energy the more circular the orbit, and in this case wouldn't the orbit be more negative than circular itself?
What is the value for Vmin after the star's mass doubles?
 
  • #7
Well

Vmin=-1/2(.k^2*m)/(L^2*r^2)

We know that the new k=2*GMm

But we know that k^2/r^2=4U^2

So Vmin=-4/2U^2m/(m^2v^2)

Vmin=-4/2U^2/(U)




which is -2U

That is less than the new energy, which is -3/2U

So it is eliptical because they are different but E is more but is still negative.
 
  • #8
D H said:
No, it isn't. Torque is not needed and does not answer the question. For example, invoking torque as an explanation does not explain why the radial component of velocity doesn't instantaneously change.

I don't get this though. If there is a sudden change of potential, there is a sudden change of force - doesn't that constitute an impulse?
 
  • #9
marmot said:
So it is eliptical because they are different but E is more but is still negative.
Correct.

marmot said:
I don't get this though. If there is a sudden change of potential, there is a sudden change of force - doesn't that constitute an impulse?
No. The force undergoes a step change, not a delta function. Jerk (time derivative of force) is a delta function.
 
  • #10
D H said:
Correct.


No. The force undergoes a step change, not a delta function. Jerk (time derivative of force) is a delta function.

Oh so basically, you are saying that if there is an abrupt and discontinous change of force - like some mass magically doubling, that is not impulse? If the mass just kept growing continuously then it would exert an impulse right?

Sorry for being a dummy!
 
  • #11
Then two perfectly rigid billiard balls collide the balls undergo an instantaneous change in momentum. Since force is the time derivative of momentum, that means that the contact force is instantaneous infinite at the instant the balls collide and zero at all other times. This is an example of an impulsive force. Impulsive forces can be useful fictions. (Fictions because force is always finite in reality, useful because they simplify away a lot of unnecessary detail.)

In this case the momentum is continuous. While the time derivative (i.e., the force) undergoes a step change at the instant the mass doubled, it does not become unbounded. There is no impulsive force here. Looking at it the other way around, since the force is bounded, there are no instantaneous changes in velocity.
 

Related to How does a sudden doubling of the mass of a star affect the orbit of a planet?

1. What is the energy of planetary orbits?

The energy of planetary orbits refers to the total amount of energy that is required for a planet to maintain its orbit around the sun. This includes both the kinetic energy (movement) and potential energy (position) of the planet.

2. How is the energy of planetary orbits calculated?

The energy of planetary orbits is calculated using the formula: E = KE + PE, where E is the total energy, KE is the kinetic energy, and PE is the potential energy. The kinetic energy is calculated using the mass and velocity of the planet, while the potential energy is calculated using the mass of the planet, the mass of the sun, and the distance between them.

3. What is the relationship between energy and the shape of a planetary orbit?

The energy of a planetary orbit is directly related to the shape of the orbit. A more elongated (or eccentric) orbit will have a higher energy, while a more circular orbit will have a lower energy. This is because a more elongated orbit requires more energy to maintain the planet's position and velocity as it moves farther away from the sun.

4. How does energy affect the stability of planetary orbits?

The energy of planetary orbits plays a crucial role in determining the stability of a planet's orbit. If the energy is too high, the planet may escape its orbit and be flung out into space. On the other hand, if the energy is too low, the planet may spiral into the sun. A delicate balance of energy is needed to maintain a stable orbit.

5. Can the energy of planetary orbits change over time?

Yes, the energy of planetary orbits can change over time due to various factors such as gravitational interactions with other planets, collisions with asteroids or comets, and changes in the mass or velocity of the planet. These changes in energy can also lead to changes in the shape and stability of the orbit.

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