How Does Satellite Orbit Duration Affect Gravity Calculation?

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Homework Help Overview

The discussion revolves around calculating the acceleration due to gravity (g) at a satellite's orbit with a given orbital period (T) of 5.1 x 10^3 seconds. The context involves gravitational forces and orbital mechanics, specifically how the satellite's orbit duration relates to gravity calculations.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning, Problem interpretation, Assumption checking

Approaches and Questions Raised

  • Participants explore the relationship between gravitational force and orbital period, discussing equations related to centripetal force and gravitational attraction. Some question the adequacy of given information, particularly the lack of distance from the Earth's center. Others suggest using angular velocity and centripetal force equations to derive relationships involving g, T, and r.

Discussion Status

The discussion is active, with participants sharing various approaches and equations. Some express uncertainty about the problem's solvability due to missing information, while others provide insights into the relationships between the variables involved. There is no explicit consensus on a solution, but several productive lines of reasoning are being explored.

Contextual Notes

Participants note that the problem is presented as a multiple-choice question, which may influence their approach. There is acknowledgment of skipped topics in class, such as angular velocity, which may affect understanding of the problem.

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A satellite orbits Earth with T= 5.1 x 10^3 s. What is the value for g at this point.

some constants i found:
Mass of Earth = 5.98 x 10^24lg
r of Earth = 6.38 x10^6m

I realize that because the T is pretty small that the value for g will be close to 9.8. This is what i can think of

Gmemo / r^2 = mg
Gme / r^2 = g

and

Fc = mo4pie^2r / T^2
Since Fc = Fg

mg = mo4pie^2r / T^2
thus g = 4pie^2r / T^2

i tried subbing the equations together to get r and from that get g but it seems to me like I am doing it wrong. Its only a multiple choice problem so i don't see why it would be so complicated (if infact its done they i showed).

Thank for any help
 
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The gravitational constant (g) depends on the square of the distance from the centre of the Earth.
 
yes but your not given the distance... only the radius of earth
 
Let the force of attraction between the satelite be F. Let the mass of Earth be taken as M and G is constant of gravity while g is thevalue of acceleration due to gravity for a point situated there at a point r distance away from the surface of the Earth which has radius as R. So distance between centre of mass is R + r. Let the mass of the staelite be m.
So now by Newton's law we get, F = mg = mMG/(R + r)^2
Therefore g = MG/(R + r)^2. In this equation we have two unknowns and so the question is unsolvable from just this equation.
So let us take the equation involving the period taken to revolve around earth. It took 5100s to complete one revolution. Fromthis information, by assuming that the only Force applied on the on object is the Earth's gravitational speed while other forced are negligibe compared to this, we can say that there is no tangential acceleration along the circular path propelled by the body. Thus we get the angular velocity of the body. And from this we get the radial component of acceleration of the circle.
w = 2pi/T
F = mw^2/R + r.
g = w^2/R + r
MG/(R + r)^2 = w^2/(R + r)
MG/w^2 = R + r
Even if it is a multiple choice question I cannot think of something that will help you in this question even without solving it.
 
ahh my class skipped angular velocity maybe that's why i didn't know what to do.

thanks a bunch
 
Using the centripetal force equation one gets
[tex]F_c=\frac{mv^2}{r}[/tex]
and substituting for v
[tex]v=\frac{2\pi r}{T}[/tex]
this centripetal force is supplied by the universal gravitational force and by using the fact that
[tex]g=G\frac{M}{r^2}[/tex]
you get the required formula in terms of [itex]r,\ T[/itex]
 

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