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常规推进剂贮存远程测控系统设计
引用本文:朱丹波,左明聪,单琳.常规推进剂贮存远程测控系统设计[J].火箭推进,2014,40(4):62-66.
作者姓名:朱丹波  左明聪  单琳
作者单位:西安航天动力试验技术研究所,陕西西安,710100
摘    要:某推进剂库房为常规液体火箭发动机地面试验提供燃料和氧化剂,燃料和氧化剂均为有毒有害物质,燃料具有易燃易爆特性.为了提高推进剂贮存安全性和工艺系统操作过程安全性,便于集中控制和管理,提出了推进剂贮存库房远程测控系统设计方案.该系统符合RMS设计要求,已成功应用于推进剂库房,提高了系统安全性和自动化程度.

关 键 词:远程测控系统  安全监控  RMS设计

Design of remote measurement and control system for conventional propellant bunker
ZHU Dan-bo,ZUO Ming-cong,SHAN Lin.Design of remote measurement and control system for conventional propellant bunker[J].Journal of Rocket Propulsion,2014,40(4):62-66.
Authors:ZHU Dan-bo  ZUO Ming-cong  SHAN Lin
Institution:(Xi' an Aerospace Propulsion Test Technology Institute, Xi' an 710100, China)
Abstract:The propellant bunker provides fuel and oxidant for the rocket engine grouno test. tiotn the fuel and oxidant are all poisonous. The fuel is flammable and explosive. A design scheme of remote measurement and control system for the propellant bunker is proposed to improve the security of propellant storage and convenience of the operation process. The system has been successfully used in the propellant bunker, and matches with the design requirements of RMS. It improved the security and the degree of automatization.
Keywords:remote measurement and control system  security monitoring  RMS design
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