An artificial satellite is revolving around a planet of mass M and radius R in a certain orbit of radius r. Using dimensional analysis show that the period of satellite . where K is a dimensionless constant and G is acceleration due to gravity.
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we know from Kepler's 3rd law, The square of the orbital period of a planet is directly proportional to the cube of the semi-major axis of its orbit.
if T is orbital period of satellite and r is the semi major axis of its orbit then,
Now suppose ,
or, , where A is proportionality constant
or, [T²] = A[L³] [L]^x [LT^-2]^y
or, [T²] = A[L^(3 + x + y) T^-2y]
compare both sides,
-2y = 2 => y = -1
3 + x + y = 0 => 3 + x - 1 = 0=> x = -2
so, T² = Ar³R^-2g^-1
or, T² = Ar³/R²g
taking square root both sides,
, k = √A
so,
if T is orbital period of satellite and r is the semi major axis of its orbit then,
Now suppose ,
or, , where A is proportionality constant
or, [T²] = A[L³] [L]^x [LT^-2]^y
or, [T²] = A[L^(3 + x + y) T^-2y]
compare both sides,
-2y = 2 => y = -1
3 + x + y = 0 => 3 + x - 1 = 0=> x = -2
so, T² = Ar³R^-2g^-1
or, T² = Ar³/R²g
taking square root both sides,
, k = √A
so,
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