Questions
A satellite of mass m revolving in a circular orbit of radius r around the earth of mass M has a total energy E. Then its angular momentum will be :
detailed solution
Correct option is C
Velocity of the satellite is GMr, angular momentum L =mvrL= mGMr r =mGMr----1given total energy -GMm2r= E⇒GM=2ErmNow, substituting the value of GM in 1L=m2Ermr=2Er2mTalk to our academic expert!
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The masses, each of mass m are kept on the vertices of an equilateral triangle of side a. Find the work needed to be done to change the length of the triangle twice of its original value.
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