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A rocket is launched vertically from the surface of earth with an initial velocity `v`. How far above the surface of earth it will go? Neglect the air resistance.A. `(R_(E)v^(2))/(gR_(E)-v^(2))`B. `(R_(E)v^(2))/(gR_(E)+v^(2))`C. `(R_(E)v^(2))/(2gR_(E)-v^(2))`D. `(R_(E)v^(2))/(2gR_(E)+v^(2))` |
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Answer» Correct Answer - C ( c) Let the rocket reaches a height h from the surface of earth. Total energy at the surface of the earth is `E_(s)=(1)/(2)mv^(2)-(GM_(E)m)/(R_(E))` where m and `M_(E)` are the masses of rocket and earth respectively. At highest point, the velocity of the rocket becomes zero. `:.` Total energy at the highest point is `E_(h)=-(GM_(E)m)/((R_(E)+h))` According to law of conservation of energy, `E_(s)=E_(h)` `:.(1)/(2)mv^(2)-(GM_(E)m)/(R_(E))=-(GM_(E)m)/(R_(E)+h)` `(1)/(2)v^(2)-(GM_(E))/(R_(E))=-(GM_(E))/(R_(E)+h)` `=(gR_(E)^(2))/(R_(E))-(gR_(E)^(2))/(R_(E)+h)( :. G=(GM_(E))/(R_(E)^(2)))` `=gR_(E)(1-(R_(E))/(R_(E)+h))=gR_(E)((h)/(R_(E)+h))` `v^(2)(R_(E)+h)=2gR_(E)h` `v^(2)R_(E)=2gR_(E)h-v^(2)h` `R_(E)v^(2)=h(2gR_(E)-v^(2))` `h=(R_(E)v^(2))/(2gR_(E)-v^(2))` |
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