To solve the problem of finding the time period of rotation of the satellite that is 9 times closer to the Earth than the Moon, we can use Kepler's Third Law of Planetary Motion. Kepler's Third Law states:
\(\frac{T_1^2}{T_2^2} = \frac{R_1^3}{R_2^3}\)
Where:
Given that the satellite is 9 times closer to the Earth than the Moon, we have:
We are given:
Substituting the given values into Kepler’s Third Law equation:
\(\frac{T_1^2}{27^2} = \frac{\left(\frac{1}{9}R_2\right)^3}{R_2^3}\)
Simplify the equation:
\(\frac{T_1^2}{27^2} = \frac{1}{9^3}\)
\(\frac{T_1^2}{729} = \frac{1}{729}\)
Solve for \(T_1\):
\(T_1^2 = 1\)
\(T_1 = \sqrt{1}\)
Thus, \(T_1 = 1 \text{ day}\).
The correct answer is 1 day.
This calculation shows that when a satellite is 9 times closer to Earth compared to the Moon, its time period of rotation is 1 day, as per Kepler's Third Law.
The height from Earth's surface at which acceleration due to gravity becomes \(\frac{g}{4}\) is \(\_\_\)? (Where \(g\) is the acceleration due to gravity on the surface of the Earth and \(R\) is the radius of the Earth.)