JEE Main & Advanced AIEEE Solved Paper-2013

  • question_answer
    What is the minimum energy required to launch a satellite of mass m from the surface of a planet of mass M and radius R in a circular orbit at an altitude of 2R?     AIEEE Solevd Paper-2013

    A) \[\frac{5GmM}{6R}\]                    

    B) \[\frac{2GmM}{3R}\]    

    C)        \[\frac{GmM}{2R}\]       

    D)        \[\frac{GmM}{3R}\]  

    Correct Answer: A

    Solution :

    The kinetic energy at altitude\[2R=\frac{GMm}{6R}\] The gravitational potential energy at altitude \[2R=-\frac{GMm}{3R}\] \[\therefore \]Total energy\[=k\varepsilon +PE=-\frac{GMm}{6R}\] Potential energy at the surface is \[-\frac{GMm}{R}\] \[\therefore \]Req. kinetic energy                 \[=\frac{GMm}{R}-\frac{GMm}{6R}=\frac{5GMm}{6R}\]


You need to login to perform this action.
You will be redirected in 3 sec spinner