A planet moves in an elliptical orbit around the sun. The mass of the sun is M_s. The minimum and maximum distances of the planet from the sun are R_1 and R_2 , respectively.
Using Kepler's 3rd law and Newton's law of universal gravitation, find the period of revolution ,P, of the planet as it moves around the sun. Assume that the mass of the planet is much smaller than the mass of the sun.
Express the period in terms of G, M_s, R_1, R_2.
T^2 = 4(pi)^2(r)^3 / GM
The Attempt at a Solution
r = (R_1 + R_2 ) / 2
T^2 = [ 4 pi^2 * ( 1/2 (R_1+R_2) ) ^3 ] / GM
T = sqrt ( " the above" );
I guess I went wrong somewhere. any help?