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If mass density of earth varies with distance 'r' from centre of earth as rho = kr and 'R' isradius of earth, then find the orbital velocity of an object revolving around earth at adistance '2R' from its centre. |
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Answer» `sqrt((pikR ^(3)G)/(4))` ![]() Let 'M' be total mass of EARTH. Consider a shell of thickness 'DR' and mass 'DM' at a distance 'r' from centre inside earth, `implies dm = rho 4 pi x ^(2) dr ` `M int dm` `= underset(0) overset(R ) int 4 pi kr^(3) dr` `=(4 pi k R ^(4))/(4) = pi kR ^(4)` Let field due to earth's gravity at a distance '2R' from centre be `T.IxxA=4 pi G m _("inside).` `impliesIxx 4pi (2R) ^(2) =4 pi G (pi kR^(4))` `impliesI =(pikR ^(4)G)/(4R^(2))` `implies I =(pi k R ^(4) G )/(4R^(2)) ` For a satellite of mass 'm' MOVING in orbit of '2R' RADIUS. `mI =(mv^(2))/((2R))` `implies I =(V^(2))/(2R)` `implies (pi kR ^(2)G)/(4) =(V^(2))/(2R)` `V = sqrt((pi kR ^(5)G)/(2))` |
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