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A planet is revolving round the sun in elliptical orbit. Its closest distance is r and farthest distance is R. If the orbital velocity closestto the sun is v, then velocity v at farthest point is : |
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Answer» `(vr)/(R )` `therefore I_(1)omega_(1)=I_(2)omega_(2) or MR_(1)^(2)omega_(1)=MR_(2)^(2)omega_(2)` Now `omega_(1)=(v)/(r ) and omega_(2)=(V)/(R )` `therefore r^(2)xx (v)/(r )=R^(2)xx(V)/(R ) or vr=V.R` or `V=(vr)/(R )`. CORRECT choice is (a). |
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