摘要
对支撑熔盐膜法脱除航天舱中CO2进行了详细的研究,实验考察了熔盐膜端电压与操作电流间的关系,探讨了电流密度、阴极室CO2浓度、气体流量等因素对CO2传质通量及脱除率的影响。
In this paper, the experimental study was made on CO_2 removal from cabin gas of spacecraft using supported molten salt membrane method.The experimental qrantities,such as the electric current density,the concentration of CO_2 and the gas flow rate in cathode conpartnent are tested.
出处
《郑州大学学报(工学版)》
CAS
1998年第S1期33-38,共6页
Journal of Zhengzhou University(Engineering Science)
基金
国家自然科学基金
河南省杰出青年科学基金
关键词
支撑熔盐膜
二氧化碳
脱除
实验
supported molten salt membrane method
carbon dioxide
removal
experiment