Architecture Design of Distributed Solid Rocket Motor Integrated System

  • Xinping Fan
  • , Ran Wei
  • , Xiao Hou
  • , Siyuan Gou
  • , Yifan Ma

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

Abstract

During the solid rocket motor (SRM) design process, multiple adjustments are necessary to meet the technical specifications defined by the overall design department and to optimize the solution. Existing design systems face challenges such as difficulties in integrating algorithm modules, limited system extensibility, and inadequate computational acceleration. To address these issues, this paper introduced a distributed cluster computing approach, established a standardized algorithm module interface specification, conducted a data interaction mechanism. Based on these foundations, A distributed integrated computing system, SRMstudio clusters, was developed to perform parallel computations for large-scale parameter combinations. successfully identifying optimal parameter combinations that satisfied the overall requirements. The proposed algorithm integration standards, data interaction mechanisms, and distributed framework facilitate efficient exploration of the design space, providing substantial data support for SRM design.

Original languageEnglish
Title of host publicationAeronautical, Aerospace and Mechanical Engineering - Proceedings of the 8th International Conference, AAME 2025
EditorsJohn P.T. Mo
PublisherIOS Press BV
Pages173-183
Number of pages11
ISBN (Electronic)9781643686363
DOIs
StatePublished - 27 Nov 2025
Event8th International Conference on Aeronautical, Aerospace and Mechanical Engineering, AAME 2025 - Suzhou, China
Duration: 28 Mar 202530 Mar 2025

Publication series

NameAdvances in Transdisciplinary Engineering
Volume82
ISSN (Print)2352-751X
ISSN (Electronic)2352-7528

Conference

Conference8th International Conference on Aeronautical, Aerospace and Mechanical Engineering, AAME 2025
Country/TerritoryChina
CitySuzhou
Period28/03/2530/03/25

Keywords

  • architecture
  • distributed
  • integrated
  • solid rocket motor

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