Enterprise electricity moon phase energy storage

What are the energy requirements for a lunar mission?

The energy requirements (which can be thermal and/or electrical) of a lunar mission are determined by several factors such as the landing site, lunar environment, span and profile of the missions, and whether it is robotic and/or manned. The energy requirements include the needs of both power generation and storage.

Can an ISRU-based system store heat and generate electricity for lunar missions?

We present a trade-off analysis of the options identified for an ISRU-based system to store heat and generate electricity for lunar missions with both robotic and human activities. A critical review of the energy requirements for a mission scenario consisting of long duration stays on the lunar surface has been carried out.

Does a lunar surface economy need an electric power utility?

This especially true as a lunar surface economy begins and requires an electric power utility. VI. ACKNOWLEDGMENTS The authors would like to thank NASA’s Space Technology Mission Directorate, Game Changing Development Program for funding this work.

Could a lunar ISRU-based thermoelectric plant fulfill the power requirements?

A trade-off analysis of the technologies and components that could be used in a lunar ISRU-based thermoelectric plant that fulfills the power requirements for settlement missions has been presented. The requirements have been established from the analysis of previous works and missions.

Can a lunar microgrid be used as a power source?

A similar approach can be taken for the lunar surface. A lunar microgrid would offer the ability to integrate various power sources to maximize power availability, including nuclear, solar arrays, batteries, and regenerative fuel cells.

What are the components of Lunar ISRU energy storage and electricity generation system?

Therefore, the following set of components is proposed for the lunar ISRU energy storage and electricity generation system: Linear Fresnel reflectors →Pumped fluid loop →Sintered regolith block with metal fins →Pumped fluid loop →Stirling engine →Pumped fluid loop →Radiator with solar shield Fig. 3 shows the configuration of the proposed system.