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[" The additional linetic energy to be p...

[" The additional linetic 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 "],[R_(1)" to another of radius "R_(2)(R_(2)>R_(1))" is "],[[" (1) "GmM((1)/(R_(1))-(1)/(R_(2)))," (2) "2GmM((1)/(R_(1)^(2))-(1)/(R_(2)^(2))],[" (3) "(1)/(2)GmM((1)/(R_(1))-(1)/(R_(2)))," (4) GmM "(1)/(R_(1)^(2))-(1)/(R_(2)^(2))]]

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