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A satellite is moving around the earth w...

A satellite is moving around the earth with speed v in a circular orbit of radius r. IF the orbit radius is decreased by 1%, its speed will

A

increase by 1%

B

increase by 0.5 %

C

decrease by 1%

D

decrease by 0.5 %

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The correct Answer is:
To solve the problem step by step, we will use the relationship between the speed of a satellite in a circular orbit and the radius of that orbit. ### Step 1: Understand the relationship between speed and radius The speed \( v \) of a satellite in a circular orbit of radius \( r \) is given by the formula: \[ v = \sqrt{\frac{GM}{r}} \] where \( G \) is the gravitational constant and \( M \) is the mass of the Earth. ### Step 2: Differentiate the equation To find how the speed changes when the radius changes, we can take the logarithm of both sides: \[ \log v = \frac{1}{2} \log G + \frac{1}{2} \log M - \frac{1}{2} \log r \] Differentiating both sides with respect to \( r \): \[ \frac{d(\log v)}{dt} = 0 + 0 - \frac{1}{2} \frac{d(\log r)}{dt} \] This simplifies to: \[ \frac{dv}{v} = -\frac{1}{2} \frac{dr}{r} \] ### Step 3: Express the percentage change Now, we can express the percentage change in speed \( \delta v \) in terms of the percentage change in radius \( \delta r \): \[ \frac{\delta v}{v} = -\frac{1}{2} \frac{\delta r}{r} \] Multiplying both sides by 100 gives us: \[ \delta v \% = -\frac{1}{2} \delta r \% \] ### Step 4: Substitute the given change in radius We are given that the orbit radius is decreased by 1%. Therefore: \[ \delta r \% = -1\% \] Substituting this into our equation: \[ \delta v \% = -\frac{1}{2} \times (-1\%) = 0.5\% \] ### Step 5: Conclusion Thus, the speed of the satellite will increase by 0.5% when the orbit radius is decreased by 1%. ### Final Answer The speed of the satellite increases by 0.5%. ---

To solve the problem step by step, we will use the relationship between the speed of a satellite in a circular orbit and the radius of that orbit. ### Step 1: Understand the relationship between speed and radius The speed \( v \) of a satellite in a circular orbit of radius \( r \) is given by the formula: \[ v = \sqrt{\frac{GM}{r}} \] where \( G \) is the gravitational constant and \( M \) is the mass of the Earth. ...
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