The additional kinetic energy to be provided to a satellite of mass m revolving around a planet of mass M, to transfer it from a circular orbit of radius R1 to another of radius R2 (R2 > R1) is
- GmM ( 1R12- 1R22 )
- GmM ( 1R1- 1R2 )
- 2GmM ( 1R1- 1R2 )
- 12GmM ( 1R1- 1R2 )
Answer
(4) 12GmM ( 1R1- 1R2 )
Solution
Total energy of a satellite in a circular orbit of radius R: E = - GMm2R
Energy to be supplied = E2 - E1
= - GMm2R2 - (- GMm2R1 )
= 12GmM ( 1R1- 1R2 )
Answer: (4)