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XJTU-REF 液体火箭发动机故障仿真数据集解读

Translated title of the contribution: XJTU-REF liquid rocket engine fault simulation datasets: a tutorial
  • Xi'an Jiaotong University
  • National Key Lab of Aerospace Power System and Plasma Technology

Research output: Contribution to journalArticlepeer-review

Abstract

Reusable launch vehicles are the most effective means and prerequisite to greatly reduce the cost of space launch and realize large-scale space applications. Fault diagnosis can improve the reliability, overall safety and sustainability of reusable engines. For all kinds of current diagnosis methods,the lack of a standard engine fault database for unified testing and evaluation restricts the theoretical research and engineering application of liquid rocket engine fault diagnosis technology. In order to solve the above problems,mathematical modeling and fault simulation experiments were carried out,and the obtained experimental data set was released to scholars around the world. The dataset contains 19 engine signals under 10 operating conditions, including normal operating conditions and valve failure, combustion chamber failure, gas generator line failure, turbo pump failure, and other fault conditions. The dataset has rich fault types and detailed recorded information, which can provide fresh data support for the fault diagnosis research of liquid rocket engine and help the progress and development of reusable launch vehicle technology.

Translated title of the contributionXJTU-REF liquid rocket engine fault simulation datasets: a tutorial
Original languageChinese (Traditional)
Pages (from-to)917-925
Number of pages9
JournalZhendong Gongcheng Xuebao/Journal of Vibration Engineering
Volume39
Issue number4
DOIs
StatePublished - Apr 2026
Externally publishedYes

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