A satellite is orbiting just above the surface of the earth with period T. If d is the density of the earth and G is the universal constant of gravitation, the quantity Gd3π represents:
A
T
B
T
C
T2
D
T3
Step-by-Step Solution
Time Period Formula: The time period T of a satellite orbiting very close to the surface of the Earth (radius R) is given by:
T=2πGMR3
Squaring both sides:
T2=GM4π2R3
Substitute Mass with Density: Assuming the Earth is a sphere of uniform density d, mass M=Volume×Density=34πR3d.
Derivation: Substitute the expression for M into the T2 equation:
T2=G(34πR3d)4π2R3T2=34πGR3d4π2R3
Canceling 4π, R3 terms:
T2=31Gdπ=Gd3π
Thus, the quantity Gd3π represents T2.
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