Calculating orbital radius and speed of an asteroid in the asteroid belt

AI Thread Summary
The discussion centers on calculating the orbital radius and speed of an asteroid in the asteroid belt, which has a period of 4.2 Earth years. The initial attempt to solve for the radius used an incorrect value for gravitational acceleration, applying Earth's g instead of the universal gravitational constant G. There is confusion regarding the correct application of Kepler's laws, specifically the equation T = 2π√(r/g), which was misapplied. Participants emphasize the need to reference proper gravitational constants and review relevant materials for accurate calculations. Understanding Kepler's laws is crucial for solving the problem correctly.
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Homework Statement



The asteroid belt circles the sun between the orbits of Mars and Jupiter. One asteroid has a period of 4.2 Earth years. What are the asteroid's orbital radius and speed?

Homework Equations



T = 2pi sqrt(r/g)

The Attempt at a Solution



I tried manipulating the above equation to solve for r. I got 4.383, but it was wrong.
 
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I used 9.81 for the value of g.
 
Why did you do that? You need to use the universal gravitational constant G, not the Earth's standard gravitational acceleration, g. Moreover, this equation,

T = 2\pi \sqrt{\frac r g}

is not quite. What are Kepler's laws?
 
I have no idea. We didn't discuss them in depth.
 
You were trying to use one of Kepler's laws here,

T = 2\pi \sqrt{\frac r g}

but you did it wrong. Where did you get that equation from? Look over your text and your notes.
 
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