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Match the Column I with Column II For a satellite in circular orbit (where `M_(E)` is the mass of the earth , m is the mass of the satellite and r is the radius of the orbit )A. A-r, B-s,C-q,D-pB. A-q,B-p,C-r,D-sC. A-p,B-q,C-s,D-rD. A-s,B-r,C-p,D-q |
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Answer» Correct Answer - D (d) Kinetic energy `=(GM_(E)m)/(2r),A-s` Potential energy `=-(GM_(E)m)/( r),B-r` Total energy `=-(GM_(E)m)/(2r),C-p` Orbital velocity `=sqrt((GM_(E))/( r)),D-q` |
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