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Model Correction and Uncertainty Evaluation of Pressure Measurement for Liquid Rocket Engine

  • Junya Fang
  • , Qingbo Li
  • , Sirui Ling
  • , Chun Cao
  • , Lei Zhou*
  • , Yunzhi Huang
  • *Corresponding author for this work
  • Beijing Institute of Aerospace Testing Technology
  • Space Experiment Technology Division

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

This study investigates outlier detection and influence factor analysis for the pressure measurement system of a liquid rocket engine. Based on the results of the influence factor analysis, the pressure measurement model is corrected. Concurrently, uncertainty analysis procedures based on the GUM (Guide to the Expression of Uncertainty in Measurement), Monte Carlo, and Bayesian methods are established for both the uncorrected and corrected models, along with comparative analyses. The research findings reveal that the corrected pressure values are higher than the uncorrected values, while the uncertainty results are comparable. Furthermore, when the engine test data exhibit a non-normal distribution, the Monte Carlo and Bayesian methods yield smaller uncertainty estimates compared to the GUM approach.

Original languageEnglish
Title of host publicationProceedings of 2025 International Conference of Mechanical Engineering on Aerospace, CoMEA 2025
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9798331599171
DOIs
StatePublished - 2025
Event2025 International Conference of Mechanical Engineering on Aerospace, CoMEA 2025 - Harbin, China
Duration: 20 Jun 202522 Jun 2025

Publication series

NameProceedings of 2025 International Conference of Mechanical Engineering on Aerospace, CoMEA 2025

Conference

Conference2025 International Conference of Mechanical Engineering on Aerospace, CoMEA 2025
Country/TerritoryChina
CityHarbin
Period20/06/2522/06/25

Keywords

  • Liquid rocket engine
  • model correction
  • pressure measurement
  • uncertainty evaluation

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