1.

What is the time period of satellite near the earth's surface? (neglect height of the orbit of satellite from the surface of the earth)?

Answer»

Solution :The force on the satellite due to earth is given by `F=(GmM)/(R^(2))`
M-Mass of earth `=6xx10^(24) kg`
m-mass of satellite,
R-radius of earth `=6.4xx10^(6) m`
Let v be the speed of the satellite
`v=(2pi R)/(T) RARR T=(2 pi R)/(v)`
Required CENTRIPETAL force is provided to satellite by the gravitational force hence
`F_(C )=(MV^(2))/(R)`
But `F_(C)=(GMm)/(R^(2))` ACCORDING to Newton.s law of gravitation.
i.e., `(GMm)/(R^(2))=(m(2pi R)^(2))/(T^(2)R)`
`rArr T^(2) =(4 pi^(2) R^(3))/(GM)`, as mass of the earth (M) and G are constants the value of T depends only on the radius of the earth.
`rArr T^(2) alpha R^(3)`
Substituting the values of M, R and G in above equation we get, T = 84.75 minutes. Thus the satellite revolving around the earth in a circular path near to the earth.s surface takes 1Hour and 24.7 minutes approximately to complete one revolution around earth.


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