Planetary Motion, calculation of orbital period

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The discussion centers on calculating the orbital period of a space shuttle orbiting Earth at a specific distance. The gravitational field strength is given as 8.9 N/kg, and the participant is confused about using two different equations for the calculation. It is clarified that while the equation r^3/T^2 is a constant for objects orbiting a particular mass, it is not equivalent to gravitational field strength (g) and lacks the correct dimensions. The correct approach involves using the equation g = 4π²R/T² for accurate results. Understanding the distinction between these formulas is crucial for solving orbital period problems correctly.
Stevo_evo_22
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Hi everyone,



I'm really confused with a particular question:

Homework Statement






A space shuttle orbits the Earth at 6720 km from its centre. The gravitational field strength is 8.9N/kg. Calculate the shuttle's orbital period in minutes...

Homework Equations



g=4pi^2 x R /T^2

The Attempt at a Solution


The thing is, I know how to solve it using g=4pi^2 x R /T^2, but I want to know why I can't just use g=r^3/T^2 (the constant for all objects orbiting a particular mass)...if I have r and g, why can't i just use this equation?

Thanks!

Steve
 
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Because r^3/T^2 is a constant. But that constant isn't the same as g. It doesn't even have the right dimensions.
 
Dick said:
Because r^3/T^2 is a constant. But that constant isn't the same as g. It doesn't even have the right dimensions.

ahh ok...thanks :)
 
The book claims the answer is that all the magnitudes are the same because "the gravitational force on the penguin is the same". I'm having trouble understanding this. I thought the buoyant force was equal to the weight of the fluid displaced. Weight depends on mass which depends on density. Therefore, due to the differing densities the buoyant force will be different in each case? Is this incorrect?

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