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Q.

A launching vehicle carrying an artificial satellite of mass m is set for launch on the surface of the earth of mass M and radius R. If the satellite is intended to move 
in a circular orbit of radius 7R, the minimum energy required to be spent by the launching vehicle on the satellite is (Gravitational constant = G) [Manipal 2012]

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a

GMmR

b

13GMm14R

c

GMm7R

d

GMm14R

answer is B.

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Detailed Solution

The energy of artificial satellite at the surface of the earth,

E1=-GMmR

When the satellite is intended to move in a circular orbit of radius 7R, then energy of artificial satellite,

E2=-12GMm7R

The minimum energy required,

E=E2-E1=GMmR-12GMm7R

=14GMm-GMm14R

=13GMm14R

 

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