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A satellite of mass m revolves around the earth of radius R at a hight x from its surface. If g is the acceleration due to gravity on the surface of the earth, the orbital speed of the satellite isA. `gx`B. `(gR^(2))/(R+x)`C. `(gR^(2))/(R+x)`D. `(gR)/(R-x)` |
Answer» Correct Answer - B `V_(0)=sqrt((GM)/(R+h))=sqrt((gR^(2))/(R+x))` |
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