MCQOPTIONS
Saved Bookmarks
| 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 | |