A satellite is orbiting just above the surface of the earth with period T. If d is the dependent of the earth and G is the universal constant of gravitation, the quantity 3π/Gd respectively:
T2
T3
\(\sqrt{T}\)
T
To solve this physics problem, we need to determine which quantity among the given options is equivalent to \(3\pi/Gd\) based on the orbital period of a satellite, denoted as \(T\), orbiting just above the Earth's surface. Let's break down the problem step-by-step:
This demonstrates that the expression \(3\pi/Gd\) is proportional to \(T^2\) in the context of a satellite orbit above the Earth's surface using Kepler's third law and the dimensions involved.
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.)