- #1
Kolahal Bhattacharya
- 135
- 1
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?
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?