SAE technical papers on CD-ROM/SAE technical paper series · 2005 · 10 citations · 3 references
EngineeringChemical EngineeringEnvironmental EngineeringEnergy SystemsHeat TransferWastewater TreatmentAdsorption ProcessesCarbon Dioxide RemovalCarbon Dioxide SeparationCompressionCompressor SystemsMolecular Sieve MembranesMolecular Sieve SeparationTemperature Swing AdsorptionThermal Balance CouplingThermal Coupling
<div class="htmlview paragraph">Continuous removal of carbon dioxide is one of the most critical processes in a spacecraft air revitalization system. Recovery of the waste carbon dioxide and its subsequent conversion to oxygen become essential for long-duration human space missions beyond Low-Earth orbit where re-supply of consumables such as oxygen is neither practical nor economical. The current CO<sub>2</sub> removal technology employed in the United States Operating Segment (USOS) of the International Space Station (ISS) operates in an open loop mode where the waste CO<sub>2</sub> is vented to space. A compressor is required to facilitate CO<sub>2</sub> recovery capabilities. The CO<sub>2</sub> removal process itself is one of the most energy-intensive processes in the life support system of the ISS due to the water vapor recovery method involved in the process. This paper discusses the design and development of a low-power CO<sub>2</sub> removal system that has capabilities to recover and compress the CO<sub>2</sub> for recycling oxygen. The system utilizes processors with no rapidly moving parts to improve the factors such as life, safety and reliability. Significant power savings is possible by incorporating a membrane dryer for water vapor recovery. Additional savings in power is achieved by thermally integrating the CO<sub>2</sub> removal and compression systems.</div>
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James C. Knox, David F. Howard · SAE technical papers on CD-ROM/SAE technical paper series · 1999 · 12 citations
Engineering, Aerospace Engineering, Mechanical Engineering +13