Find the radius of a geo-stationary satellite

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To determine the radius of a geo-stationary satellite in terms of Earth's radius (R_e), the equation M_s*w^2*R_s=G*M_e*M_s/R_s^2 is used, leading to R_s^3=gR_e^2/w^2. The angular velocity (w) can be calculated, but the challenge lies in deriving the specific ratio of R_s to R_e, which Kleppner states is 6.6. The discussion suggests that plugging in numerical values may be necessary to achieve this relationship, as an algebraic solution is not readily apparent. Ultimately, the focus is on understanding the calculations involved in finding the radius of a geo-stationary satellite.
Kolahal Bhattacharya
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To find the radius of a geo-stationary satellite in terms of R_e, we see---

M_s*w^2*R_s=G*M_eM_s/R_s^2 from where using GM_e=g R_e^2,

We get R_s^3=gR_e^2/w^2. w can be evaluated. The problem is because of the fact that
Kleppner provides the soln. R_s=6.6R_e.How, one can get rid of fractional exponent?
 
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My guess is that you have to plug in the numbers, and then in the end get the 6.6 relationship. I don't see an algebraic way to do it offhand.
 
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