Simulation Study of Environmental Control and Life Support System Design for Deep Space Exploration

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dc.creatorMoroshima, Reiji
dc.creatorMoriyama, Eriko
dc.creatorTerao, Takuma
dc.creatorTaguchi, Ayako
dc.creatorHirosaki, Tomofumi
dc.creatorEshima, Samuel
dc.creatorMiyajima, Hiroyuki
dc.date.accessioned2019-06-20T17:44:54Z
dc.date.available2019-06-20T17:44:54Z
dc.date.issued2019-07-07
dc.descriptionReiji Moroshima, Space Systems Development Corporation (SSD), Japan
dc.descriptionEriko Moriyama, Space Systems Development Corporation (SSD), Japan
dc.descriptionTakuma Terao, Space Systems Development Corporation (SSD), Japan
dc.descriptionAyako Taguchi, Space Systems Development Corporation (SSD), Japan
dc.descriptionTomofumi Hirosaki, Space Systems Development Corporation (SSD), Japan
dc.descriptionSamuel Eshima, University of Colorado Boulder (CU Boulder), USA
dc.descriptionHiroyuki Miyajima, International University of Health and Welfare (IUHW), Narita Campus, Japan
dc.descriptionICES301: Advanced Life Support Systems Control
dc.descriptionThe 49th International Conference on Environmental Systems was held in Boston, Massachusetts, USA on 07 July 2019 through 11 July 2019.
dc.description.abstractWith Japan participating in the Lunar Orbital Platform-Gateway (LOP-G) program, expectations to use the LOP-G as an advanced base to open the door to deep space will increase and further destinations for human spaceflight will likely to be planned. This derives the need to design an environmental control and life support system (ECLSS) that can withstand a long duration mission without resupplies. In particular, an atmosphere revitalization (AR) subsystem and a water recovery and management (WRM) subsystem require highly reliable architectures with higher regeneration rates than ones currently operating in the International Space Station (ISS), as well as an environmental monitoring and control subsystem demands advanced technologies with great efficiency. We have worked for years to develop SICLE (SImulator for Closed Life and Ecology), a software to design and simulate ECLSS models, based on the knowledge of ECLSS simulations at the Closed Ecology Experiment Facilities (CEEF) in Japan. In addition, our recent research and development of ECLSS assemblies including carbon dioxide removal, oxygen generator and water recovery and management with JAXA has contributed largely to the development of SICLE. This paper discusses the results of the ECLSS simulation analyses using SICLE especially on water/air revitalization, temperature, humidity, and CO2 concentration control of the space habitat currently designed for deep space exploration.
dc.format.mimetypeapplication/pdf
dc.identifier.otherICES_2019_244
dc.identifier.urihttps://hdl.handle.net/2346/84459
dc.language.isoeng
dc.publisher49th International Conference on Environmental Systems
dc.subjectECLSS
dc.subjectLife Support System
dc.subjectDeep Space Exploration
dc.subjectSICLE
dc.subjectAtmosphere Revitalization
dc.subjectWater Recovery and Management
dc.titleSimulation Study of Environmental Control and Life Support System Design for Deep Space Explorationen_US
dc.typePresentations

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