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[1]王文龙,赵政社,混 平,等.液体火箭发动机地面试车应变数据采集系统研制[J].火箭推进,2011,37(03):52-59.
　WANG Wen-long,ZHAO Zheng-she,HUN Ping,et al.Development of strain parameter acquisition system for liquid rocket engine ground testing[J].Journal of Rocket Propulsion,2011,37(03):52-59.
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液体火箭发动机地面试车应变数据采集系统研制

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 37 期数: 2011年03期 页码: 52-59 栏目: 测控与试验 出版日期: 2011-06-15
Title:
Development of strain parameter acquisition system for liquid rocket engine ground testing
文章编号:
1672-9374(2011)03-0052-08
作者:
王文龙; 赵政社; 混 平; 耿 直
西安航天动力试验技术研究所，陕西 西安 710100
Author(s):
WANG Wen-long;  ZHAO Zheng-she;  HUN Ping;  GENG Zhi
Xi’an Aerospace Propulsion Test Technique Institute, Xi’an 710100, China
关键词:
载人航天; 运载火箭; 液体火箭发动机; 推进技术
Keywords:
manned space flight;  launch vehicle;  LRE;  data acquisition system
分类号:
V434-33
文献标志码:
A
摘要:
针对液体火箭发动机地面试车应变参数测试原理和需求，研制了应变数据采集系统。对系统的硬件集成方式、软件开发策略进行了介绍，重点阐述系统集成中的难点、软件开发中的关键技术突破。调试与试验验证结果证明，系统稳定可靠、满足研制要求。
Abstract:
A new strain data acquisition system was developed according to the testing principle and requirement of strain parameters in the liquid rocket engine (LRE) ground testing. particular describing The hardware integration mode and software exploitation strategyof the system are introduced. The difficulties of the system integration and the key technologies are elaborated emphatically. The debugging and testing results show that the new system is steady and reliable, and can meet the requirement of system development.

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备注/Memo

收稿日期：2010-10-13；修回日期：2010-11-15
基金项目：中国航天科技集团公司支撑项目
作者简介： 王文龙（1982—），男，工程师，研究领域为研究领域为发动机测试

更新日期/Last Update: 1900-01-01