Calculate Mercury's Orbital Speed and Distance: Universal Gravity Equation

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Homework Help Overview

The discussion revolves around calculating Mercury's distance from the Sun at perihelion using its orbital speed at aphelion and perihelion. The subject area includes concepts from celestial mechanics and gravitational physics.

Discussion Character

  • Conceptual clarification, Mathematical reasoning, Problem interpretation

Approaches and Questions Raised

  • Participants explore the conservation of energy approach to relate kinetic and potential energy at different points in Mercury's orbit. There are attempts to derive the distance at perihelion based on given velocities and distances at aphelion.

Discussion Status

Some participants have offered alternative equations and methods for calculating the perihelion distance, while others are questioning the correctness of the equations being used. There is ongoing exploration of the assumptions behind the energy conservation approach.

Contextual Notes

Participants are discussing the implications of using equations for circular orbits versus elliptical orbits, indicating a need to clarify the conditions under which these equations apply. There is also uncertainty regarding the treatment of kinetic energy at perihelion.

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Homework Statement



Mercury's orbital speed varies from 38.8km at aphelion to 59.0km at perihelion.

If the planet is 6.60*10^10m from the Sun's center at aphelion, how far is it at perihelion?

Homework Equations



v = sqrt(GM/r) (speed,circular orbit)


The Attempt at a Solution



V_a = velocity of aphelion = 38.8km = 3.88 * 10^4m
V_p = velocity of perihelion = 59.0km = 5.9 * 10^4m


V_a = sqrt(GM/r)

3.88 * 10^4m = sqrt(GM/r_a)
and solving for M gives me (I think)

M = (3.88 * 10^4m*r_a)^2 / G


V_b = sqrt(GM/r_p) ; where W_b = 5.9 * 10^4m

solving for r_p gives :

r_p = (3.88 * 10^4m *r_a ) / 5.9 * 10^4m

; where r_a = 6.60*10^10m;

and

r_p = 4.60 * 10^10

is this right?
 
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Since Mercury travels in an ellipse you shouldn't be using an equation for velocity in a circular orbit. What you want to do is to use the fact that total energy is conserved. That is,

KE (Perihelion) + PE (perihelion) = KE (aphelion) + PE (aphelion)

Once you express these energies in their proper form, you will see that you have only one unknown -- the distance at perihelion.
 
Is this the right equation ;

KE (Perihelion) + PE (perihelion) = KE (aphelion) + PE (aphelion)

0 - GMm/ r_e = 1/2 mv^2 - GMm/r_a

and solving for r_e I get (check it )

r_e = GM / (1/2 v^2) - r_a

and plug in the numbers now, if this is correct
 
Last edited:
anyone?
 
tnutty said:
Is this the right equation ;

KE (Perihelion) + PE (perihelion) = KE (aphelion) + PE (aphelion)

0 - GMm/ r_e = 1/2 mv^2 - GMm/r_a

and solving for r_e I get (check it )

r_e = GM / (1/2 v^2) - r_a

and plug in the numbers now, if this is correct

How did you get that KE at perihelion was 0?
 
ok wait here is what i think is correct,

KE (Perihelion) + PE (perihelion) = KE (aphelion) + PE (aphelion)

1/2*mv^2 - GMm/ r_e = 1/2 mv^2 - GMm/r_a

= (check this below?)

r_e = -GMm / (1/2mV_a^2 - GMm/r_a -1/2mV_p^2 )

r_e = -GM / (.5V_a^2 - GM/r_a - .5V_p^2 )

r_e = 4.598 * 10^10
 
I guess that is correct but I have 1 question :

KE (Perihelion) + PE (perihelion) = KE (aphelion) + PE (aphelion)

it does not matter if

the above formual is switch right, the perihelion on the right side and
the aphelion on the left?
 

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