How to Calculate the Orbital Period of a Satellite Around Planet Zeta?

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Homework Help Overview

The discussion revolves around calculating the orbital period of a satellite around the fictitious planet Zeta. The problem involves gravitational forces and orbital mechanics, with a specific focus on the relationship between the radius of orbit and the period of the satellite.

Discussion Character

  • Exploratory, Assumption checking, Problem interpretation

Approaches and Questions Raised

  • Participants discuss the use of gravitational equations to relate the orbital period of the satellite to that of the moon Eta. There is uncertainty regarding the application of the formula and the calculations leading to the period of the satellite.

Discussion Status

Some participants have provided guidance on the calculations, suggesting the need to take the square root of a derived value. However, there is ongoing confusion about the expected answer and the orbital radius, with multiple interpretations being explored.

Contextual Notes

Participants question the accuracy of the provided answer and consider the possibility of a typographical error in the problem statement. There is also mention of an impending exam, adding urgency to the discussion.

EskShift
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A satellite is being prepared for take-off on the surface of the fictitious planet Zeta. The planet Zeta has a radius of R and the satellite experiences a gravitational force, F, from the planet at the surface. A single moon, Eta, completes one orbit of the planet every 50 days at a distance of 5R from the center of the planet.
The satellite is now placed into orbit 2R from the surface of the planet.

Determine the Period of the satellite.


Homework Equations


Well i assume you use (R^3 / T^2)A = (R ^ 3 / T ^ 2)B



The Attempt at a Solution


Therefore
5R ^3 / 50^2 = 3R^2 / T^2
T is what we need, but i seem to always get 540 and am not exactly sure as to how to work it out.
Am i using the wrong equation? or is my working out wrong?

thanks.
 
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EskShift said:
A satellite is being prepared for take-off on the surface of the fictitious planet Zeta. The planet Zeta has a radius of R and the satellite experiences a gravitational force, F, from the planet at the surface. A single moon, Eta, completes one orbit of the planet every 50 days at a distance of 5R from the center of the planet.
The satellite is now placed into orbit 2R from the surface of the planet.

Determine the Period of the satellite.

Homework Equations


Well i assume you use (R^3 / T^2)A = (R ^ 3 / T ^ 2)B

The Attempt at a Solution


Therefore
5R ^3 / 50^2 = 3R^2 / T^2
T is what we need, but i seem to always get 540 and am not exactly sure as to how to work it out.
Am i using the wrong equation? or is my working out wrong?

thanks.

Welcome to PF.

Don't you need to take the square root of 540?
 
LowlyPion said:
Welcome to PF.

Don't you need to take the square root of 540?

I thought so too, but that is approximately 23. The answer says 40 days? I still don't understand what I'm doing wrong, and i have an exam tomorrow!
 
Working backwards from 40 days that suggests an orbital radius of 4.3R from the center doesn't it?
 
LowlyPion said:
Working backwards from 40 days that suggests an orbital radius of 4.3R from the center doesn't it?

It certainly does, possibly the answer is a miss-type, everyone i have asked have all said they don't understand. but i haven't asked my teacher yet, he might know. but ill be happy if my working is correct at least?
 
EskShift said:
It certainly does, possibly the answer is a miss-type, everyone i have asked have all said they don't understand. but i haven't asked my teacher yet, he might know. but ill be happy if my working is correct at least?

Perhaps there is a misstatement in the problem?
 

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