Systems and methods for lunar utility with navigation, advanced remote sensing, and autonomous beaming for energy redistribution

A lunar structure comprising:

• a base comprising legs to couple to a planetary body;
• a retractable mast coupled to the base, the retractable mast comprising deployable interlocking actuated bands and a bellow, wherein the deployable interlocking actuated bands extend away from the base, and wherein the bellow surrounds the retractable mast;
• a payload coupled to a top portion of the retractable mast, the payload comprising a plurality of individual housing portions that are each configured to store an operational component;
• a solar power system coupled to the top portion of the retractable mast, the solar power system configured to extend downward from the top portion of the retractable mast and collect solar energy;
• a thermal dissipation system coupled to the retractable mast and the base, the thermal dissipation system configured to expel thermal energy from the payload to an external environment;
• and
• a thermal consolidation system coupled to the retractable mast, the thermal consolidation system configured to maintain thermal energy in an enclosure that surrounds the base.