1velocity must be greater then orbital velocity and must be less then escape velocity, i think you can now solve the rest!!!!!!!!!!!
a satellite is in a circular orbit very close to the surface of a planet. at some point it is given an impulse along its direction of motion, causing the vel to increase by μ times. it now moves in an elliptical orbit with the planet at the center of the ellipse.
the max possible value of μ is : :
1) 2
2) √2
3) √2-1
4)1/(√2 - 1)
-
UP 0 DOWN 0 0 5
5 Answers
1
