How is orbital energy transferred between celestial bodies?

In summary, orbital energy can be transferred via gravitational encounters, such as in the case of a space probe being slingshotted by Jupiter. During this interaction, the probe's velocity is increased and its orbit is changed due to the transfer of energy and angular momentum from Jupiter. This concept is explained by considering the exchange of momentum between the two objects involved. Additionally, the concept of conservation of angular momentum plays a role in this process, as the total angular momentum of the system remains constant despite the transfer of momentum between objects.
  • #1
dschmidt12
9
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I know that I have learned this at some point in my past and that I am probably just blanking on the explanation, but I have been having some trouble remembering just how orbital energy is transferred via gravitational encounters (for example, between stars in a binary system). Physically, how is this explained? Also, how does the concept of conservation of angular momentum play into this? Again, I know this is probably simpler than I am making it out to be in my mind; I just wanted to make sure I remembered the reason.
 
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  • #2
dschmidt12 said:
I know that I have learned this at some point in my past and that I am probably just blanking on the explanation, but I have been having some trouble remembering just how orbital energy is transferred via gravitational encounters (for example, between stars in a binary system). Physically, how is this explained? Also, how does the concept of conservation of angular momentum play into this? Again, I know this is probably simpler than I am making it out to be in my mind; I just wanted to make sure I remembered the reason.
Think first about the Earth-moon system. Moon gravity creates tides and dissipates energy on the Earth. The moon has orbital angular momentum, and the Earth has rotational angular momentum. The only conserved quanty is angular momentum, independent of the rate of energy dissipation.
Bob S
 
  • #3
dschmidt12 said:
[...] I have been having some trouble remembering just how orbital energy is transferred via gravitational encounters (for example, between stars in a binary system). Physically, how is this explained? Also, how does the concept of conservation of angular momentum play into this?

You use the word 'encounters', which leads me to think you that what you have in mind is the example of gravitational assist, a short duration interaction. (Wikipedia is a good place to start with reading about gravity assist.) Then again, you also mention the case of stars in a binary system, and that's not an encounter, but a continuous interaction; your question is somewhat ambiguous.

Bob S has said some things about tidal interaction, I will say some things about gravitational assist.


Take the case of a space probe, on route to Jupiter, in such a way that on fly-by a gravitational slingshot will take the probe to Saturn.

If you zoom into a local picture, the probe on a fly-by heading, then to a good approximation the trajectory of the probe is along a hyperbola. Within the scope of that local picture Jupiter and the probe exchange momentum. The direction of motion of the probe is changed by the interaction with Jupiter, and that is reciprocal, the momentum of Jupiter is changed proportionally.

If you zoom out to the scale of Jupiter's orbit you need to take into account that Jupiter and the probe are in individual orbits in the solar system, so angular mechanics applies.

The probe doesn't approach Jupiter "head on", the probe is on a course that makes it "overtake" Jupiter from behind. (Also, Jupiter's orbit is concentric, while the probe's orbit is highly eccentric.)

During the phase of significant gravitational interaction between Jupiter and the probe Jupiter is in a sense "towing" the probe, increasing its orbital energy.

After the fly-by, when the distance between Jupiter and the probe has increased so much that the gravitation between them is negligable compared to the Sun's gravitation their motion can be thought of as individual orbits again. Some of Jupiter's angular momentum has been transferred to the probe, and some orbital energy has been transferred.

Cleonis
 
  • #4
Cleonis said:
You use the word 'encounters', which leads me to think you that what you have in mind is the example of gravitational assist, a short duration interaction. (Wikipedia is a good place to start with reading about gravity assist.) Then again, you also mention the case of stars in a binary system, and that's not an encounter, but a continuous interaction; your question is somewhat ambiguous.

Bob S has said some things about tidal interaction, I will say some things about gravitational assist.


Take the case of a space probe, on route to Jupiter, in such a way that on fly-by a gravitational slingshot will take the probe to Saturn.

If you zoom into a local picture, the probe on a fly-by heading, then to a good approximation the trajectory of the probe is along a hyperbola. Within the scope of that local picture Jupiter and the probe exchange momentum. The direction of motion of the probe is changed by the interaction with Jupiter, and that is reciprocal, the momentum of Jupiter is changed proportionally.

If you zoom out to the scale of Jupiter's orbit you need to take into account that Jupiter and the probe are in individual orbits in the solar system, so angular mechanics applies.

The probe doesn't approach Jupiter "head on", the probe is on a course that makes it "overtake" Jupiter from behind. (Also, Jupiter's orbit is concentric, while the probe's orbit is highly eccentric.)

During the phase of significant gravitational interaction between Jupiter and the probe Jupiter is in a sense "towing" the probe, increasing its orbital energy.

After the fly-by, when the distance between Jupiter and the probe has increased so much that the gravitation between them is negligable compared to the Sun's gravitation their motion can be thought of as individual orbits again. Some of Jupiter's angular momentum has been transferred to the probe, and some orbital energy has been transferred.

Cleonis

Yes, I did mean gravitational assist; I'm sorry for being so ambiguous. :) I believe that I understand the concept now, however, I just wanted to make sure that my understanding of the matter was correct. In the case of Jupiter and the probe, during the gravitational force that Jupiter exerts on the probe transfers energy to the probe, thus increasing its velocity by accelerating it. Since angular momentum is also being transferred, the radius of the probe's orbit must also increase, thus changing the orbit of the probe. Thank you so much for all of your help!
 
  • #5
Bob S said:
Think first about the Earth-moon system. Moon gravity creates tides and dissipates energy on the Earth. The moon has orbital angular momentum, and the Earth has rotational angular momentum. The only conserved quanty is angular momentum, independent of the rate of energy dissipation.
Bob S

Ah, thanks, I believe that I understand that now. :)
 

1. What is the concept of "transferral of orbital energy"?

The concept of "transferral of orbital energy" refers to the exchange of energy between objects in orbit, such as planets, moons, and satellites. This can occur through various mechanisms, such as gravitational interactions or the use of propulsion systems.

2. How does the transfer of orbital energy affect the motion of objects in space?

The transfer of orbital energy can greatly impact the motion of objects in space. For example, a gravitational slingshot maneuver can increase the speed of a spacecraft by transferring energy from a planet's orbit. Conversely, a spacecraft can use a propulsion system to transfer energy to a planet and slow down its own orbit.

3. Can the transfer of orbital energy be controlled?

Yes, the transfer of orbital energy can be controlled through the use of various methods and technologies. For instance, spacecraft can use precision maneuvers and calculations to accurately transfer energy between orbits. Additionally, advanced propulsion systems can be used to control the amount and direction of energy transfer.

4. What are some real-world applications of the transfer of orbital energy?

The transfer of orbital energy has many practical applications in space exploration and technology. For example, it is used for spacecraft navigation and trajectory planning, as well as for satellite communications and imaging. It also plays a crucial role in the functioning of our solar system, as planets and moons transfer energy to maintain their orbits.

5. Are there any potential risks or drawbacks to the transfer of orbital energy?

There are potential risks and drawbacks to the transfer of orbital energy, particularly in terms of spacecraft operations. If not executed properly, energy transfers can result in collisions or undesired changes in orbit. Additionally, certain types of energy transfer, such as gravitational slingshots, can have long-term effects on the orbits of planets and other objects in space.

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