Study on virtual test technology of liquid propellant engine

DUAN Na; ZHANG Li-hui; XU Shan-shan; ZHU Zi-huan; YU Hai-lei

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Study on virtual test technology of liquid propellant engine

更新时间：2026-07-07

- Study on virtual test technology of liquid propellant engine
- Vol. 25, Issue 7, (2010)
- 作者机构：
  
  1. 北京航空航天大学宇航学院,北京,100191
  2. 中国航天科技集团公司航天推进技术研究院北京航天试验技术研究所,北京,100074
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2010
- 稿件说明：
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DUAN Na, ZHANG Li-hui, XU Shan-shan, et al. Study on virtual test technology of liquid propellant engine[J]. 2010, 25(7).
DOI：

DUAN Na, ZHANG Li-hui, XU Shan-shan, et al. Study on virtual test technology of liquid propellant engine[J]. 2010, 25(7). DOI：

摘要

设计了虚拟试验平台的框架结构

开发了面向对象的映射型数据库系统

分析了试验管理器模块的实现流程

阐述了建模仿真模块、虚拟环境模块等关键功能模块的研制过程

通过多种接口机制将多种技术集成为一个无缝计算机环境.最后

举例进行说明

并总结了虚拟试验技术应用到液体火箭发动机试验的优势.

Abstract

The framework of the virtual test bed was designed.Objective/relationship mapping storage structure database system was developed

and the implementation flow of test management was analyzed.The development process of modeling and simulation module and virtual environment module was mainly explained.Then

the unique collaborative computing environment was developed via various interfaces

and the examples were given.At last

the advantages of applying virtual test in liquid rocket engine were concluded.

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Related Author

Jun TIAN

Yufan XIE

Fei LONG

Qin LIU

Yidan CHEN

Hongyu CHEN

Yazhou LIU

Dengfeng LIU

Related Institution

China Special Vehicle Research Institute，Aviation Industry Corporation of China，Limited

Airport Support Bureau，Air Force Logistics Department

Nanjing Puguo Technology Company，Limeted

National Key Laboratory of Science and Technology on Liquid Rocket Engines，Xi'an Aerospace Propulsion Institute，China Aerospace Science and Technology Corporation

Laboratory of Science and Technology on Cryogenic Liquid Propulsion，Beijing Aerospace Propulsion Institute，China Aerospace Science and Technology Corporation

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