Part 1. I would do the same as above for saying launching to the east in the same direction as the Earth etc. but I would add u locate the launch site for the rocket closest to the equator, because there is the greatest rotational motion there because as velocity = distance /time, because a place at equator has to cover more distance because the circumference of earth is biggest there in the rotation in the same time (24 hours), the velocity has to be greater. Then link this to making it more economical because less fuel is needed and a greater velocity is obtained.
Part 2. Yeah the q is weird saying evaluate, normally it's an explain or describe, so if it was describe I would do this for the 4 marks. Define what g-force is: g - force is a convenient way to express the contact force on astronaut in multiples of what they would normally experience on earth (gforce = 1 + a/g). Then discuss like the different stages. Prior to launch: the rocket is stationary on the launchpad therefore there is no acceleration and thus a g force of 1 is experience. During lift-off: remains constant at 1 g force, until the thrust of the rocket overcomes the weight force, and at this point the g force experienced is slightly greater than one. From here on: as fuel is expended the mass of the rocket decreases, and as a = T-mg/m by newtons 2nd law, as acceleration is inversely proportional to mass of rocket, the acceleration of the rocket increases and thus gforce also increases. However, in multi stage rockets, when all fuel is expended in one rocket stage the rocket momentarily is in free fall and thus at this point a g force of 0 is experience. Also, at peaks of the g force a human can safely withstand engines are momentarily shut off to ensure safety of astronauts.