1.

A satellite is revolving in a circular orbit at a height 'h' from the earth's surface (radius of earth R, h lt lt R). The minimum increases in its orbital velocity required, so that the satellite could escape from the earth's gravitational field, is close to : (Neglect the effect of atmosphere)

Answer»

`SQRT(GR)( sqrt(2)-1)`
`sqrt(2gR)`
`sqrt(gR)`
`sqrt(g(R )/(2))`

ANSWER :A


Discussion

No Comment Found