Dynamics of Uniform Circular Motion Quesiotn

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Homework Help Overview

The problem involves a satellite in a circular orbit around a planet, with specific parameters such as mass, orbital radius, and period. The question seeks to determine the true weight of the satellite when it is at rest on the planet's surface.

Discussion Character

  • Exploratory, Assumption checking, Conceptual clarification

Approaches and Questions Raised

  • Participants discuss the relationship between mass and weight, with one noting that mass remains constant regardless of location. There is confusion regarding the correct radius to use in gravitational equations, and questions arise about how to calculate the weight of the satellite on the planet's surface.

Discussion Status

Some participants have provided guidance on how to approach finding the mass of the planet and the gravitational attraction at the surface. There is an ongoing exploration of the concepts of mass versus weight, and the discussion reflects a mix of interpretations and attempts to clarify the problem setup.

Contextual Notes

Participants are working under the constraints of a homework problem, which may limit the information available for solving the question. There is an emphasis on understanding the definitions of mass and weight, as well as the implications of using different radii in calculations.

kraigballa
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Homework Statement



A satellite has a mass of 5700 kg and is in a circular orbit 4.2 multiplied by 10^5 m above the surface of a planet. The period of the orbit is two hours. The radius of the planet is 4.25 multiplied by 10^6 m. What is the true weight of the satellite when it is at rest on the planet's surface?

Homework Equations



G = gravitational constant
Me = Mass of planet
r1 = radius from planet to satellite
r2 = radius of planet
v = velocity of satellite in orbit
Fc = centripetal force
T = Time

Fc = msat*v^2/r


G*msat*Me/r^2 = msat*v^2/r

v = Sq. Root(G*Me/r)

The Attempt at a Solution



r1 = 4.67e^6
r2 = 4.25e^6

T = 7200seconds

so v1 = 2*pie*r1/T = 4075.343803 m/s

so Me = v^2 * r1/G = 1.1628389e^24

not sure how to find mass of satellite on planet from here...
 
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The mass of the satellite on the planet is the same as everywhere else, 5700 kg. That's only part of your problem. When you say

G*msat*Me/r^2 = msat*v^2/r

what did you use for r? It'd better be r1+r2, the distance from the center of the planet not the surface.
 
Yeah for r1 I did the radius of the planet plus the radius of the satellite.

So it should be 5700 kg up in orbit and still 5700 kg on the planets surface? Edit: I guess the answer is supposed to be in "N"
 
kraigballa said:
Yeah for r1 I did the radius of the planet plus the radius of the satellite.

So it should be 5700 kg up in orbit and still 5700 kg on the planets surface? Edit: I guess the answer is supposed to be in "N"

Don't confuse mass with weight. Mass is the same everywhere, but "weight" is the force with which the planet attracts the satellite near its surface. Mass is expressed in kilograms and weight in Newtons. Do you know how to find the weight?
 
I am not sure how to find weight...? With the given problem that is
 
You can find the mass of the planet when the satellite is in orbit from the given quantities. Then put the satellite at rest on the surface of the planet and find the gravitational attraction at that point. That is the weight.
 

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