Understanding the Meaning of 'p' in Equation: p^2 = (4pi^2)(a^3)/G(m1+m2)

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In summary, the equation discussed represents Kepler's Third Law and is used to calculate the orbital period of two objects based on their masses and distance. The variable 'p' represents the orbital period in seconds, and is calculated by taking the square root of the right side of the equation. Other variables in the equation stand for the semi-major axis, gravitational constant, and masses of the two objects. This equation is fundamental in orbital mechanics and is used to understand and predict the motion of objects in space. However, it can only be used for circular orbits and not for other types of orbits.
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aerogurl2
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hi, there's something that i don't understand in the following equation:

p^2 = (4pi^2)(a^3)/G(m1+m2)

is the p a distance measured from the center of the first object to the center of the second object? or is it just the distance between them, for example a satelitte dish is 300km above the Earth's surface, so would p be 300km or 300km+radius of earth?
 
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http://www.allrefer.com/kepler-s-laws-of-planetary-motion"
 
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Hello,

Thank you for your question. In this equation, 'p' represents the orbital period of the two objects, which is the time it takes for them to complete one orbit around each other. It is not a distance measurement, but rather a measure of time.

To answer your question, the value of 'p' would depend on the specific context of the problem. If the objects are orbiting around each other at a distance of 300km above the Earth's surface, then the value of 'p' would be the time it takes for them to complete one orbit at that specific distance. However, if the objects are orbiting at a different distance, the value of 'p' would change accordingly.

I hope this helps clarify the meaning of 'p' in this equation. If you have any further questions, please let me know. Thank you.
 

1. What does the variable 'p' represent in this equation?

The variable 'p' represents the orbital period, which is the time it takes for an object to complete one full orbit around another object.

2. How is the value of 'p' calculated in this equation?

The value of 'p' is calculated by taking the square root of the right side of the equation, which is equal to (4pi^2)(a^3)/G(m1+m2). This value represents the orbital period in seconds.

3. What do the other variables in the equation stand for?

'a' represents the semi-major axis, which is half the distance between the two objects. 'G' is the gravitational constant, 'm1' and 'm2' are the masses of the two objects, and 'pi' is a mathematical constant representing the ratio of a circle's circumference to its diameter.

4. How is this equation used in orbital mechanics?

This equation, known as Kepler's Third Law, is used to calculate the orbital period of two objects based on their masses and distance. It is a fundamental equation in orbital mechanics and is used to understand and predict the motion of objects in space.

5. Can this equation be used for any type of orbit?

No, this equation is specifically for circular orbits. For other types of orbits, such as elliptical or parabolic, different equations would need to be used.

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