Two satellites s and s' revolve around the earth at distance 3R and 12R from the Centre of the earth. The periods of revolution of s and s' are in ratio of
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Explanation:
given that,
s and s' satellite revolving around the earth
therefore,radius of s satellite= 3R
and radius of s' satellite= 12R
we know that,
(T1/T2)^2 = (r1/r2)^3
(T1/T2)^2 = ( 3R /12R)
(T1/T2)^2=(1R/4R)
therefore, taking square root both the sides
(T1/T2) = 1/2
therefore, T1:T2 = 1:2
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