Gravitation and its effect on elliptical orbits

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Homework Help Overview

The discussion revolves around the gravitational effects on the speed of a comet in an elliptical orbit as it moves between two distances from the sun. The original poster presents a problem involving the calculation of the comet's speed at a specific distance, referencing gravitational principles and energy conservation.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning

Approaches and Questions Raised

  • Participants explore the relationship between speed and distance in elliptical orbits, referencing the conservation of angular momentum and energy. They discuss setting up equations based on the areas swept out by the comet and attempt to derive formulas for calculating the speed at different distances.

Discussion Status

Multiple approaches have been proposed, including using conservation of energy and angular momentum principles. Participants are actively refining their equations and calculations, with some expressing uncertainty about their results while others provide corrections and suggestions for improvement.

Contextual Notes

There is mention of specific distances and initial speeds, but the discussion also highlights the lack of clarity regarding terms like perihelion and aphelion. Participants are working within the constraints of the problem as presented, without additional context or data beyond what is provided in the homework statement.

marekkpie
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Homework Statement



Comets travel around the sun in elliptical orbits with large eccentricities. Suppose the comet has an initial speed of 1.17*10^4 m/s when at a distance of 4.9*10^11 m from the center of the sun, what is its speed when at a distance of 5.9*10^10 m? Give your in m/s in scientific notation to three significant digits. (Note: Use appendix F for the necessary data.)

Homework Equations



Don't know 'em. All I know is finding velocity in a circular orbit:

v = sqrt((Gravitational constant * mass of the object being orbited around) / radius from the center of the orbited object)

The Attempt at a Solution



v = sqrt((6.67E-11 * 1.99E30) / 5.9E10) = 4.74E4

The correct answer is: 6.40E4...so since I'm in the same order of magnitude I assume I'm close.
 
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Orbits sweep out equal areas in equal times
Consider the area of a triangle swept by the comet in 1 sec (eg some time short enough that you can make the path a straight line) when it's far and close to the sun.

If the area is the same and you know the height you cna work out how long the base is and so the speed.
 
O.K...so since the times and areas are equal, we can safely set both sides to equal the area of a triangle? i.e.

.5 * R1 * V1 = .5 * R2 * V2
thus,
V2 = V1 * R1 / R2

But then I get 9.72E4.
 
mgb_phys said:
Orbits sweep out equal areas in equal times
Consider the area of a triangle swept by the comet in 1 sec (eg some time short enough that you can make the path a straight line) when it's far and close to the sun.

If the area is the same and you know the height you cna work out how long the base is and so the speed.

There was no mention of
perihelion or aphelion.

Conservation of energy is what is expected

David
 
Last edited:
Alright, then here is what I got from davieddy's help:

K + U = K + U

MC = mass of the comet

MS = mass of the sun

G = gravitational constant

So...here is my equation, followed by the steps to make it solve for V2:

.5 * MC * V1 ^ 2 - G * MS * MC / D1 = .5 * MC * V2 ^ 2 - G * MS * MC / D2
<=>
.5 * V1 ^ 2 - G * MS / D1 = .5 * V2 ^ 2 - G * MS * D2
<=>
...bunch of algebra...
<=>
V2 = (V1 ^ 2 + .5 * G * MS (D2 ^ -1 - D1 ^ -1)) ^ .5

which leaves me with 3.36E4. Still in the right ballpark, but not quite there.
 
marekkpie said:
V2 = (V1 ^ 2 + .5 * G * MS (D2 ^ -1 - D1 ^ -1)) ^ .5

which leaves me with 3.36E4. Still in the right ballpark, but not quite there.

Try
V2 = (V1 ^ 2 + 2 * G * MS (D2 ^ -1 - D1 ^ -1)) ^ .5
 
davieddy said:
Try
V2 = (V1 ^ 2 + 2 * G * MS (D2 ^ -1 - D1 ^ -1)) ^ .5

D'oh! Tyvm.
 

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