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PhysicsMediumMCQ2002 ยท Unknown

Q22.Energy required to move a body of mass m from an orbit of radius 2R to 3R is (1) GMm/12R2 (2) GMm/3R2 (3) GMm/8R (4) GMm/6R

What This Question Tests

This question requires calculating the change in the total mechanical energy of a satellite as it moves between two different circular orbits, using the formula for total orbital energy.

Concepts Tested

Gravitational potential energyTotal mechanical energy in orbitEnergy conservation

Formulas Used

E = -GMm/2r

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