1.

The total energy of a satellite having mass m orbiting around the earth has mass M in a circular orbit with velocity v is

Answer»

`(1)/(2) mv^(2)`
`-(1)/(2) mv^(2)`
`m v^(2)`
`(GMm)/(8)`

Solution :As `K.E. = (1)/(2) mv^(2) = (1)/(2)m(GM)/(R ) = (GMm)/(2R)`
`P.E. = (-GMm)/(r ) = - mv^(2)`
`T.E. = K.E. + P.E.`
`= (1)/(2) mv^(2) - mv^(2) = -(1)/(2) mv^(2)`


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