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A satellite orbiting Earth at an orbital radius r has a velocity v. Which represents the velocity if the satellite is moved to...Question
A satellite orbiting Earth at an orbital radius r has a velocity v. Which represents the velocity if the satellite is moved to an orbital radius of 5r?(1 point)
Responses
A) 1/5√v
the fraction with numerator 1 and denominator square root of 5 v
B) 1/5v
1 fifth v
C) √5v
square root of 5 v
D) 5v
Responses
A) 1/5√v
the fraction with numerator 1 and denominator square root of 5 v
B) 1/5v
1 fifth v
C) √5v
square root of 5 v
D) 5v
Answers
There are no human answers yet.
Answered by
GPT-4o mini
To determine the velocity of a satellite in orbit as its orbital radius changes, we can use the formula for the orbital velocity of a satellite in a circular orbit, which is given by:
\[
v = \sqrt{\frac{GM}{r}}
\]
where:
- \( v \) is the orbital velocity,
- \( G \) is the gravitational constant,
- \( M \) is the mass of the Earth,
- \( r \) is the orbital radius.
If we denote the initial orbital radius as \( r \) and the corresponding velocity as \( v \), then:
\[
v = \sqrt{\frac{GM}{r}}
\]
Now, if the satellite is moved to an orbital radius of \( 5r \), we can find the new velocity \( v' \):
\[
v' = \sqrt{\frac{GM}{5r}} = \sqrt{\frac{1}{5}} \sqrt{\frac{GM}{r}} = \frac{1}{\sqrt{5}} v
\]
Thus, the velocity at the new radius (5r) is:
\[
v' = \frac{1}{\sqrt{5}} v
\]
This means that the correct answer is:
**A) \( \frac{1}{5\sqrt{v}} \)**
However, because A) as written seems incorrect, the expression should actually indicate that the velocity is proportional to \( \frac{1}{\sqrt{5}} v \), so none of the options in the list perfectly matches this conclusion.
If the intended meaning of option A may have a contextual error on representation, the final expression shows that the new orbital velocity is indeed \( \frac{1}{\sqrt{5}}v \), aligning closest with Option A as needing clarification. Thus, please check the representation carefully against the options provided.
\[
v = \sqrt{\frac{GM}{r}}
\]
where:
- \( v \) is the orbital velocity,
- \( G \) is the gravitational constant,
- \( M \) is the mass of the Earth,
- \( r \) is the orbital radius.
If we denote the initial orbital radius as \( r \) and the corresponding velocity as \( v \), then:
\[
v = \sqrt{\frac{GM}{r}}
\]
Now, if the satellite is moved to an orbital radius of \( 5r \), we can find the new velocity \( v' \):
\[
v' = \sqrt{\frac{GM}{5r}} = \sqrt{\frac{1}{5}} \sqrt{\frac{GM}{r}} = \frac{1}{\sqrt{5}} v
\]
Thus, the velocity at the new radius (5r) is:
\[
v' = \frac{1}{\sqrt{5}} v
\]
This means that the correct answer is:
**A) \( \frac{1}{5\sqrt{v}} \)**
However, because A) as written seems incorrect, the expression should actually indicate that the velocity is proportional to \( \frac{1}{\sqrt{5}} v \), so none of the options in the list perfectly matches this conclusion.
If the intended meaning of option A may have a contextual error on representation, the final expression shows that the new orbital velocity is indeed \( \frac{1}{\sqrt{5}}v \), aligning closest with Option A as needing clarification. Thus, please check the representation carefully against the options provided.
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