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Question number 11 from the Force, Circular Motion, Gravity Test in TBR Physics 1 Book
If the space station is located a distance of twice the radius of the Earth away from the surface of the Earth, the acceleration due to gravitational attraction from the Earth on the space station is:
A. one-ninth of that on Earth.
B. one-quarter of that on Earth.
C. one-half of that on Earth.
D. equal to that on Earth.
ANSWER: A
I don't understand how they reached the point where they said that the radius is 3RE? I plugged it in as twice the distance because that is what the question stated.
Explanation from book given:
To solve for the acceleration (call it g') exerted on the space station from the Earth, we use:
g'= GME/r^2
where r is the center-to-center distance between the Earth and the space station. This is a spin-off of the gravitational force equation, r for this problem is 3RE, where RE is the radius of the Earth. (Note that they stated the space station was 2RE away from the surface of the Earth. Remember to add in the radius of the Earth to get the center-to-center distance.) We do not know the mass of the Earth, nor do we know the radius of the Earth, so the best way to solve this problem is to recognize that g, the acceleration due to gravity at the Earth's surface, can be written as:
g= GME/(R^2E)
We then take the ratio of g' to g: GME/(3RE)2 : GME/(RE)^2= 1/9
If the space station is located a distance of twice the radius of the Earth away from the surface of the Earth, the acceleration due to gravitational attraction from the Earth on the space station is:
A. one-ninth of that on Earth.
B. one-quarter of that on Earth.
C. one-half of that on Earth.
D. equal to that on Earth.
ANSWER: A
I don't understand how they reached the point where they said that the radius is 3RE? I plugged it in as twice the distance because that is what the question stated.
Explanation from book given:
To solve for the acceleration (call it g') exerted on the space station from the Earth, we use:
g'= GME/r^2
where r is the center-to-center distance between the Earth and the space station. This is a spin-off of the gravitational force equation, r for this problem is 3RE, where RE is the radius of the Earth. (Note that they stated the space station was 2RE away from the surface of the Earth. Remember to add in the radius of the Earth to get the center-to-center distance.) We do not know the mass of the Earth, nor do we know the radius of the Earth, so the best way to solve this problem is to recognize that g, the acceleration due to gravity at the Earth's surface, can be written as:
g= GME/(R^2E)
We then take the ratio of g' to g: GME/(3RE)2 : GME/(RE)^2= 1/9