The time period of a simple pendulum,on a sat | vedclass

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(D) The time period $T$ of a simple pendulum is given by the formula $T = 2\pi \sqrt{\frac{l}{g_{eff}}}$,where $l$ is the length of the pendulum and $

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infinity

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(D) The time period $T$ of a simple pendulum is given by the formula $T = 2\pi \sqrt{\frac{l}{g_{eff}}}$,where $l$ is the length of the pendulum and $g_{eff}$ is the effective acceleration due to gravity.Inside an artificial satellite orbiting the Earth,the satellite and everything inside it are in a state of weightlessness,which means the effective acceleration due to gravity $g_{eff}$ is $0$.Substituting $g_{eff} = 0$ into the formula,we get $T = 2\pi \sqrt{\frac{l}{0}}$,which implies $T \rightarrow \infty$.Therefore,the time period of the pendulum is infinity.

The time period of a simple pendulum,on a satellite orbiting the Earth,is

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