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A satallite of mass `m`, initally at rest on the earth, is launched into a circular orbit at a height equal to the the radius of the earth. The minimum energy required isA. `(sqrt(3))/(4)mgR`B. `(1)/(2)mgR`C. `(1)/(4)mgR`D. `(3)/(4)mgR` |
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Answer» Correct Answer - D We know `V_(0) = sqrt((GM)/(r )) & g = (GM)/(R^(2))` From energy conservation `U_(i)+K_(i)=U_(f)+K_(f)` `-(GMm)/(R )+K_(f)=-(GMm)/(2R)+(1)/(2)mv_(0)^(1)` `K_(i)=(GMm)/(2R)+(1)/(2)m(sqrt((GM)/(2R)))^(2) rArr K_(i) = (3GMm)/(4R) rarr K_(i)=(3)/(4) mgR` |
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