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Q.

Taking the earth to be a uniform sphere of radius 6400 km and the value of g at the surface to be
10 ms2, calculate the energy needed (in × 1010J) to raise a satellite of mass 2000 kg to a height of 800 km above the earth’s surface and to set it into circular orbit at that altitude.

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answer is 7.1.

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Detailed Solution

Initial energy of the satellite,

E1=GMmR( since initial KE=o)

Final energy of the satellite

E2=GMm2(R+h)

Energy needed, ΔE=E2E1

=GMm2(R+h)GMmR=GMm1R12(R+h)

 But GM =R2g

ΔE=R2gM1R12(R+h)

=mgR1121+hR

ΔE=7.1×1010J

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