首页> 美国政府科技报告 >Lunar Module ECS (Environmental Control System) - Design Considerations and Failure Modes
【24h】

Lunar Module ECS (Environmental Control System) - Design Considerations and Failure Modes

机译:月球模块ECs(环境控制系统) - 设计考虑因素和故障模式

获取原文

摘要

Design considerations and failure modes for the Lunar Module (LM) Environmental Control System (ECS) are described. An overview of the the oxygen supply and cabin pressurization, atmosphere revitalization, water management and heat transport systems are provided. Design considerations including reliability, flight instrumentation, modularization and the change to the use of batteries instead of fuel cells are discussed. A summary is provided for the LM ECS general testing regime.

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号