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Nowadays, space crafts such as a space shuttle take the O2 gas for crew respiration from the earth. However, for long periods of stay in space and far missions such as to the moon, it is not possible to carry sufficient amounts of oxygen. Therefore, there is need to establish other methods of supplying the extra O2 required by the crew under such circumstances. The CO2 reduction system is one method to generate O2 in space.

A manned Mars mission will be undertaken in the near future. Then the need for ‘water’ will become critical. One of the solutions to the problem is making use of the resources on Mars. We take notice of CO2 reduction. The method is to generate H2O from CO2, which is major composition of Martian atmosphere. Nominally, the reaction of CO2 reduction is performed at atmospheric pressure on Earth. However, the nominal pressure of the Martian atmosphere is below 10 torr. Therefore, it is necessary to confirm whether the reaction of CO2 reduction can be performed with same efficiency as on Earth. This paper summarizes the results of a fundamental study of CO2 reduction system for a Mars mission.

Improvement of an air revitalization technology of ECLSS (Environment Control and Life Support System) is one of the key elements in development and operation of future human space systems. The paper summarizes a trace-contaminant control system which employs “thermal storage / combustion” method for reduction of cabin and equipment-generated off-gases. For comparison, the International Space Station will be equipped with a trace-contaminant system utilizing “oxidization” method with catalyst substances. Preliminary functions of the processor were also evaluated to determine the designing parameters for a space system hardware. The results indicate the capability of processor under large volumes and high concentration of trace gases, and its systematic feasibility.