Lunar development efforts continue to gain momentum, several programs are underway to achieve sustainable activities on the Moon. Therefore, there is a need for a sustainable energy supply system utilizing sunlight, which is available on the Moon. Currently, Regenerative Fuel Cell system (RFC system) are expected to develop as one of the energy supply systems. The RFC system electrolyzes the water utilizing solar power to produce hydrogen and oxygen. These generated gases are supplied to the FC system to generate electricity. The byproduct water generated during power generation is re-electrolyzed to store energy. This cycle allows the RFC system to continuously generate electricity without additional water supply. Honda has developed a high-differential-pressure water electrolysis system in parallel with the development of fuel cells system since the 1990s. In this system, protons generated by water electrolysis are transferred to the cathode side to generate high-pressure hydrogen. This creates a differential pressure across the Proton Exchange Membrane (PEM), and Honda has achieved a maximum pressure increase of 70 MPa by using its own structure. Moreover, this principle can be applied not only to the generation and pressurization of hydrogen, but also to that of oxygen. And, Honda has integrated the high-differential-pressure water electrolysis system and the fuel cell systems to develop Honda's own RFC system. Honda calls the system Circulative Renewable Energy System (CRE system). The CRE system consists of the high-differential-pressure water electrolysis system, an Electrochemical Hydrogen Compressor system (EHC system), and a fuel cell system. In the CRE system, water is first supplied to the high-differential-pressure water electrolysis system, which electrolyzes water to produce hydrogen and high-pressure oxygen. Hydrogen generated by water electrolysis is supplied to the EHC system and electrochemically pressurized. These high-pressure gases are stored in their own tanks and supplied to the fuel cell system when electricity is required. Byproduct water generated during power generation is supplied again to the water electrolysis system to enable continuous power generation. A feature of the CRE system is the pressurization of each gas, which allows them to store more gas in a smaller volume. The future gravimetric energy density of CRE systems is greater than that of a future Li-ion battery, which is thought to be advantageous in terms of helping reduce transport cost. When the CRE system is used on the Moon, fuel cells generate electricity at night when solar power is unavailable. During the daytime, hydrogen and oxygen are generated and stored by water electrolysis utilizing solar power. On the Moon, the nighttime is continuous for up to 14 days. One lunar project requires a three-year power supply, during which there will be a total of 39 lunar nights. Last year, Honda created a breadboard model for the project, and conducted 39 cycles operation test. The purpose of this cycle test was to confirm that the water could circulate and continue to generate power for 39 cycles. Several initiatives were implemented in order to complete this cycle test. For example, since the EHC system pressurize hydrogen to 70 MPa, water in the high-pressure hydrogen permeates the PEM due to differential pressure and stays in the membrane reaction part. This water causes a voltage increase. Therefore, water discharge was enhanced by optimizing the flow path structure. Another issue was the pressure increase in components that are not expected to increase internal pressure due to the movement of supply and generated gases. Therefore, we worked to build a system control that circulates the gases without external venting. As a result of this series of initiatives, it was confirmed that electricity could be generated through 39 cycles without terminating the test, and proof of principle was completed. Going forward, it will be necessary to cope with space-specific events such as vibration during launch, radiation, and low gravity. CRE system is being developed for use in lunar missions after 2030. Figure 1
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