a satellite revolves around the earth of radius R in a circular orbit of radius 3R.the % of increase in energy required to lift it to an orbit of radius 5R
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Solution
energy of satellite in the first case E1=GMm/3R energy in the second case is E2=GMm/5R ΔE=GMm/R(1/3−1/5) =GMm/R(2/15) % increase =∆E/E1×100 =2GMm/15R/GMm/3R =6/15×100=40%