Otsuji K, Hirao M, Satoh S
Mitsubishi Heavy Industries, Ltd., Nagoya Aircraft Works, Japan.
Acta Astronaut. 1987 Jan;15(1):45-54. doi: 10.1016/0094-5765(87)90065-8.
The Japanese Space Station Program is now under Phase B study by the National Space Development Agency of Japan in participation with the U.S. Space Station Program. A Japanese Space Station participation will be a dedicated pressurized module to be attached to the U.S. Space Station, and is called Japanese Experiment Module (JEM). Astronaut scientists will conduct various experimental operations there. Thus an environment control and life support system is required. Regenerable carbon dioxide removal and collection technique as well as oxygen recovery technique has been studied and investigated for several years. A regenerable carbon dioxide removal subsystem using steam desorbed solid amine and an oxygen recovery subsystem using Sabatier methane cracking have a good possibility for the application to the Japanese Experiment Module. Basic performance characteristics of the carbon dioxide removal and oxygen recovery subsystem are presented according to the results of a fundamental performance test program. The trace contaminant removal process is also investigated and discussed. The solvent recovery plant for the regeneration of various industrial solvents, such as hydrocarbons, alcohols and so on, utilizes the multi-bed solvent adsorption and steam desorption process, which is very similar to the carbon dioxide removal subsystem. Therefore, to develop essential components including adsorption tank (bed), condenser. process controller and energy saving system, the technology obtained from the experience to construct solvent recovery plant can be easily and effectively applicable to the carbon dioxide removal subsystem. The energy saving efficiency is evaluated for blower power reduction, steam reduction and waste heat utilization technique. According to the above background, the entire environment control and life support system for the Japanese Experiment Module including the carbon dioxide removal and oxygen recovery subsystem is evaluated and proposed.
日本空间站计划目前正由日本国家宇宙开发局在参与美国空间站计划的情况下进行B阶段研究。日本参与的空间站将是一个专门的加压舱,连接到美国空间站,称为日本实验舱(JEM)。宇航员科学家将在那里进行各种实验操作。因此需要一个环境控制和生命支持系统。可再生二氧化碳去除和收集技术以及氧气回收技术已经研究和调查了数年。使用蒸汽解吸固体胺的可再生二氧化碳去除子系统和使用萨巴蒂尔甲烷裂解的氧气回收子系统很有可能应用于日本实验舱。根据基本性能测试计划的结果,介绍了二氧化碳去除和氧气回收子系统的基本性能特征。还对微量污染物去除过程进行了研究和讨论。用于各种工业溶剂(如碳氢化合物、醇类等)再生的溶剂回收装置采用多床溶剂吸附和蒸汽解吸过程,这与二氧化碳去除子系统非常相似。因此,为了开发包括吸附罐(床)、冷凝器、过程控制器和节能系统在内的关键部件,从建设溶剂回收装置的经验中获得的技术可以轻松有效地应用于二氧化碳去除子系统。对风机功率降低、蒸汽减少和余热利用技术的节能效率进行了评估。根据上述背景,对包括二氧化碳去除和氧气回收子系统在内的日本实验舱整个环境控制和生命支持系统进行了评估并提出了方案。