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1. |
The radius of orbit of a geostationary satellite is given by _____ (M = Mass of the earth; R = Radius of the earth; T = Time period of the satellite) |
A. | [(T2*G*M)/(4*pi2)]3/2 |
B. | [(T2*G*M)/(4*pi2)]2/3 – R |
C. | [(T2*G*M)/(4*pi2)]1/3 – R |
D. | [(T2*G*M)/(4*pi2)]1/3 |
E. | [(T2*G*M)/(4*pi2)]3/2b) [(T2*G*M)/(4*pi2)]2/3 – Rc) [(T2*G*M)/(4*pi2)]1/3 – Rd) [(T2*G*M)/(4*pi2)]1/3 |
Answer» E. [(T2*G*M)/(4*pi2)]3/2b) [(T2*G*M)/(4*pi2)]2/3 – Rc) [(T2*G*M)/(4*pi2)]1/3 – Rd) [(T2*G*M)/(4*pi2)]1/3 | |