A satellite of mass m is launched vertically upwards with an initial speed u from the surface of the earth. After it reaches height R (R = radius of the earth), it ejects a rocket of mass m/10 so that subsequently the satellite moves in a circular orbit. The kinetic energy of the rocket is (G is the gravitational constant; M is the mass of the earth): [7-Jan-2020 Shift 1]

Question

Examsnet · Accepted Answer

Correct Answer is : 5m(u2−119200GMR)5m ≤ft( u² - 119/200 GM/R )5m(u2−200119​RGM​)

Gravitation Part 1