Hi Cindy, this question requires you to talk about all the changes in potential energy and the consequences of these chagnes. These being:
1) Earth to Earth Orbit
2) Earth Orbit to Sun Orbit then to Mars Orbit
3) Mars Orbit to Mars Surface
4) Mars surface to Mars Orbit
5) Step 2 but in reverse
6) Lowered down to Earth orbit.
Steps 1,2,4 are increases in GPE and the leftover are decreases in GPE. Also talk about g-forces experienced, the need for retroboosters when entering into Mar's atmosphere (retroboosters would be required in this process as the aim is to slow down the ship as the decrease in GPE results in increased kinetic energy and also the ship will be used again to return to Earth hence cannot simply rely only on the blunt shape of the ship and also another aspect you can talk about is that Mar's atmosphere is not as thick as Earth's so atmospheric friction isn't enough of a force to slow the ship down to safe levels)
Second part of the question refers to the charged particles emited from the Sun (KEY NOTE: they are charged particles and not limited to being +ve or -ve). There are two methods of redirecting or protecting the ship, this is through magnetic fields or electric fields. If we use an electric field, it will only repel one type of charge, hence the key note. Therefore we must use an magnetic field to protect the ships equiment from the high velocity particles. This is a very summarised answer and that question would require you to expand on this but these are the general aspects of the quesiton. Definitely encoporate many aspects of the syllabus.