How Do You Calculate Total Energy in an Elliptic Orbit?

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Homework Help Overview

The discussion revolves around deriving the total energy in an elliptic orbit, specifically the equation E = -GMm/(2a), where 'a' is the semi-major axis. Participants are exploring how to express velocity in the context of an elliptical orbit, contrasting it with the simpler case of a circular orbit.

Discussion Character

  • Exploratory, Assumption checking, Problem interpretation

Approaches and Questions Raised

  • Participants are attempting to derive the total energy equation and express velocity in an elliptical orbit. There are questions about the validity of certain formulas and whether they can be used without assuming the total energy result. Some participants suggest breaking down velocity into radial and tangential components.

Discussion Status

The discussion is ongoing, with participants sharing their thoughts and attempts to derive the necessary relationships. Some guidance has been offered regarding the use of kinetic and potential energy, but there is no explicit consensus on the approach to take.

Contextual Notes

Participants express a desire for hints rather than direct answers, indicating a preference for self-discovery in solving the problem. There are mentions of confusion regarding previous messages, suggesting a dynamic and possibly fragmented discussion.

Päällikkö
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How does one derive the total energy in an elliptic orbit:
[tex]E= - \frac{GMm}{2a}[/tex]
where a is the semi-major axis?
I did manage to get the result for the special case of circular orbit, as
[tex]v = \sqrt{\frac{GM}{R}}[/tex]

But the problem is that I can't figure out a way to express v in an elliptic orbit.

If at all possible, give hints (that is: not a direct answer), as I'd rather try it myself first :).
 
Last edited:
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Not really, no.

I can't get the given equation:
[tex]v=\sqrt{2\mu\left({1\over{r}}-{1\over{2a}}\right)}[/tex]
without assuming the result (total energy) I'm trying to get.

EDIT: Either I am getting paranoid or someone replied, but deleted his/her message :).
 
Would a formula for elliptical velocity be too much help ?
 
Fermat said:
Would a formula for elliptical velocity be too much help ?
Isn't that the equation I wrote in my second message?

I can get it by assuming
[tex]E= - \frac{GMm}{2a}[/tex]
but that's the equation I want to prove.
 
Last edited:
Päällikkö said:
...

EDIT: Either I am getting paranoid or someone replied, but deleted his/her message :).
Sorry for the confusion. That was me, then I thouight that maybe that was too much of hint - that you didn't really want !
 
Help, anyone?
 
Päällikkö said:
How does one derive the total energy in an elliptic orbit:
[tex]E= - \frac{GMm}{2a}[/tex]
where a is the semi-major axis?
I did manage to get the result for the special case of circular orbit, as
[tex]v = \sqrt{\frac{GM}{R}}[/tex]

But the problem is that I can't figure out a way to express v in an elliptic orbit.

If at all possible, give hints (that is: not a direct answer), as I'd rather try it myself first :).
The speed can be resolved into two orthogonal components - radial and tangential. Since [itex]v^2 = v_t^2 + v_r^2[/itex] (Pythagoras) the total kinetic energy is simply the sum of the tangential and radial kinetic energies. Use that, together with the fact that angular momentum and total energy is constant, to derive the relationship between radius, speed and total energy.

[tex]E(r) = KE + PE = \frac{1}{2}mv^2 - \frac{GMm}{r} = \frac{1}{2}mv_t^2 + \frac{1}{2}mv_r^2 - \frac{GMm}{r}[/tex]

Use the fact that the radial KE (middle term) is 0 when r is maximum or minimum (ie. when r = a or r=b)

AM
 

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