If a rocket is fired with a speed v=2√gR near the earth's surface and coasts upwards, its speed in the intersteller space is.
A satellite is revolving in a circular orbit at a height ‘h’ from the earth’s surface (radius of earth R ; h<<R). The minimum increase 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.)
A particle is fired vertically upward with a speed of 15 km s−1 With what speed will it move in intersteller space. Assume only earth's gravitational field.