Final answer:
For the first part of the question about the gravitational field for the given mass distributions:
- ρ(r) = k: The density is constant, so the gravitational field is also constant and is given by g = (4/3)πGk.
- ρ(r) = k/r: The density varies inversely with the distance, so the gravitational field decreases as r increases and is given by g = (4/3)πGk/r.
- ρ(r) = k/r^2: The density varies inversely with the square of the distance, so the gravitational field decreases even faster as r increases and is given by g = (4/3)πGk/r^2.
For the second part of the question about the velocity of an object in a circular orbit inside the mass distributions:
- For ρ(r) = k: The velocity of the object in a circular orbit is given by v = √(GMr).
- For ρ(r) = k/r: The velocity of the object in a circular orbit is given by v = √(GM/r).
- For ρ(r) = k/r^2: The velocity of the object in a circular orbit is given by v = √(GMr^3).
Step-by-step explanation:
The gravitational field g inside a spherical mass distribution is given by the equation g = (4/3)πGρ(r)r where G is the gravitational constant, ρ(r) is the density of the mass distribution as a function of r, and r is the distance from the center of the mass distribution.
To find the gravitational field for the given mass distributions:
- ρ(r) = k: The density is constant, so the gravitational field is also constant and is given by g = (4/3)πGk.
- ρ(r) = k/r: The density varies inversely with the distance, so the gravitational field decreases as r increases and is given by g = (4/3)πGk/r.
- ρ(r) = k/r^2: The density varies inversely with the square of the distance, so the gravitational field decreases even faster as r increases and is given by g = (4/3)πGk/r^2.
For the second part of the question about the velocity of an object in a circular orbit inside the mass distributions:
- For ρ(r) = k: The velocity of the object in a circular orbit is given by v = √(GMr).
- For ρ(r) = k/r: The velocity of the object in a circular orbit is given by v = √(GM/r).
- For ρ(r) = k/r^2: The velocity of the object in a circular orbit is given by v = √(GMr^3).