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7.Gravitation
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The value of escape velocity on a certain planet is $2\, km/s$ . Then the value of orbital speed for a satellite orbiting close to its surface is
A
$12\,km/s$
B
$1\, km/s$
C
$\sqrt 2\,km/s$
D
$2\sqrt 2\, km / s$
Solution
${v_0} = \frac{{{v_e}}}{{\sqrt 2 }} = \frac{2}{{\sqrt 2 }} = \sqrt 2 \,km/s$
Standard 11
Physics
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