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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. | [(T<sup>2</sup>*G*M)/(4*pi<sup>2</sup>)]<sup>3/2</sup> |
B. | [(T<sup>2</sup>*G*M)/(4*pi<sup>2</sup>)]<sup>2/3</sup> R |
C. | [(T<sup>2</sup>*G*M)/(4*pi<sup>2</sup>)]<sup>1/3</sup> R |
D. | [(T<sup>2</sup>*G*M)/(4*pi<sup>2</sup>)]<sup>1/3</sup> |
Answer» E. | |