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The Electron-VM Oxygen Generation System (OGS) is a main source of oxygen for crew breathing on the International Space Station (ISS) and the result of updating the Electron-V OGS that has been in successful operation for 17 years on Mir Space Station. The successful accomplishment of a manned flight program primarily has resulted in the stable operation of the system. The paper deals with analysis of off-normal situations related to the operation of the Electron-VM on board ISS. The system switching-off analysis based on the telemetry information processing and the results of the additional tests conducted under flight and ground conditions is performed. A principal cause of system switching-offs is a reduction in the pressure built by the circulating pumps due to ingress of gas bubbles into the suction pipeline. The results of the Electron-VM OGS switching-off analysis and the practical recommendations regarding its prevention are reviewed.

The Regenerative Atmosphere Revitalization and Monitoring system (ARMS), been part of Integrated Life Support System (ILSS), is intended for maintenance in the manned modules of a necessary chemical composition of an artificial gas atmosphere (AGA) on base of the crew metabolism product transform to environment initial components. Generally, the ARMS structure includes the individual systems and units intended for: → oxygen generation; → carbon dioxide removal and it concentration; → trace contaminants removal; → carbon dioxide reduction with the goal to produce an additional quantity of water necessary to increase the degree of the oxygen loop clousure. The ARMS structure of the International Space Station (ISS) Russian Segment (RS) includes the Electron-VM Oxygen Generation System (OGS), Vozdukh Carbon Dioxide Removal System (CDRS) and SBMP Trace Contaminants Removal Means (TCRM) installed in the Service Module.

The paper deals with the construction and performance data of the service module Zvezda water and oxygen supply systems of the International Space Station (ISS). The performance data at the first 14 months of manned station functioning are provided. The data of humidity condensate and recovered water compositions are reviewed. The water supply and demand balance are analyzed. The system of oxygen generation “Electron-VM” and its functioning results are reviewed. The effective cooperation of the international partners on part of life support is shown.

The paper describes the design specifics of the system for oxygen generation by electrolysis Elektron and major results obtained in long-term operation of the system aboard space station Mir. Operational data analysis makes possible to draw a conclusion that the system is capable to attain life parameters for at least 2 years with maintaining serviceability for no less than 8 years without attendance and unit replacement. Based on flight operation the possibility of reducing power consumption by 10 per cent is proven. System design updates are realized in the water electrolysis system intended for the Russian segment of the international space station.

This paper deals with a man-made Gas Atmosphere (MMGA) Simulation Model developed and software presented for the Russian Segment of the International Space Station (ISS). The simulation Model (SM) is intended for analysis of the MMGA parameter nonstationary values in isothermal and non-isothermal conditions under a variable number of crew taking into account the intensities of the crew activity. The person's structure of the SM, basic assumptions, taken for modeling and formalized descriptions of SM separate modules. Formalized descriptions by the Segment's Pressurized Modules are based on using the nonlinear equations of mass/energy balance for the controlling volume, taking into account all main sources and sinks of the environment separate components, which are a crew, Integrated Regenerative Life Support System (IRLSS) separate subsystems, ISS on-board systems.

As space flights tend to be more prolonged problems of oxygen generation by physico-chemical means assume greater importance. The paper deals with the water electrolysis process and CO2 reduction. Some operational results of the system for water electrolysis on Mir space station are presented. Expected characteristics of the systems for water electrolysis and carbon dioxide reduction are considered.

As space flights tend to be more prolonged problems of oxygen generation by physicochemical means assume greater importance. The paper deals with the water, electrolysis process, CO2 concentration and processing organisation schemes. Some operational results of the system for electrolysis of aqueous alkali solution and CO2 removal on Mir space station are presented. Expected characteristics of the complex system for oxygen generation from carbon dioxide are considered.