The configuration of the solar arrays, which collect and convert sunlight into electricity, is a key factor that affects the design of solar systems in space. Depending on the mission objectives, the orbit, and the spacecraft size and shape, different configurations have different advantages and disadvantages. Fixed arrays, for instance, are attached to the spacecraft body and do not move. They are simple, lightweight, and reliable but have limited power output and may face shading or orientation issues. Deployable arrays, on the other hand, are folded during launch and deployed after reaching orbit. They can provide more power and adjust to the optimal angle of sunlight but are more complex, heavier, and prone to mechanical failures or damage from debris or micrometeoroids. Finally, concentrator arrays use lenses or mirrors to focus sunlight onto smaller cells. While they can achieve higher efficiency and reduce the area and mass of the arrays, they require precise pointing and tracking systems and may suffer from thermal stress or degradation.