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Integrated Atmosphere Resource Recovery and Environmental Monitoring Technology Demonstration for Deep Space Exploration

机译：用于深空探测的大气资源综合回收和环境监测技术示范

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摘要

Exploring the frontiers of deep space continues to be defined by the technological challenges presented by safely transporting a crew to and from destinations of scientific interest. Living and working on that frontier requires highly reliable and efficient life support systems that employ robust, proven process technologies. The International Space Station (ISS), including its environmental control and life support (ECLS) system, is the platform from which humanity's deep space exploration missions begin. The ISS ECLS system Atmosphere Revitalization (AR) subsystem and environmental monitoring (EM) technical architecture aboard the ISS is evaluated as the starting basis for a developmental effort being conducted by the National Aeronautics and Space Administration (NASA) via the Advanced Exploration Systems (AES) Atmosphere Resource Recovery and Environmental Monitoring (ARREM) Project.. An evolutionary approach is employed by the ARREM project to address the strengths and weaknesses of the ISS AR subsystem and EM equipment, core technologies, and operational approaches to reduce developmental risk, improve functional reliability, and lower lifecycle costs of an ISS-derived subsystem architecture suitable for use for crewed deep space exploration missions. The most promising technical approaches to an ISS-derived subsystem design architecture that incorporates promising core process technology upgrades will be matured through a series of integrated tests and architectural trade studies encompassing expected exploration mission requirements and constraints.
机译：通过安全地将机组人员往返于具有科学意义的目的地之间所带来的技术挑战，继续探索深空领域。在该领域的生活和工作需要高度可靠且高效的生命支持系统，该系统采用可靠的成熟工艺技术。国际空间站（ISS）包括其环境控制和生命支持（ECLS）系统，是人类进行深空探索任务的平台。国际空间站上的国际空间站ECLS系统大气振兴（AR）子系统和环境监测（EM）技术体系结构被评估为美国国家航空航天局（NASA）通过高级探索系统（AES）进行开发工作的基础大气资源恢复和环境监测（ARREM）项目。ARREM项目采用了一种渐进的方法，以解决ISS AR子系统和EM设备，核心技术和运营方法的优缺点，以减少发展风险，改善功能ISS子系统系统的可靠性和较低的生命周期成本，适用于人员深空探测任务。通过一系列包含预期勘探任务要求和约束条件的集成测试和体系结构贸易研究，将最有希望的技术方法应用于ISS衍生的子系统设计体系结构，该体系结构融合了有希望的核心工艺技术升级。

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