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Computer aided preliminary design of propellant grains for solid rocket motors

  • Guozhu Liang*
  • , Huiyu Wang
  • , Zhongqin Zhang
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

The objective of this paper is to develope an integrated grain design computer program for computation of grain geometry, including internal ballistics, grain strength and drafting display, so as to quickly perform preliminary design of solid propellant grains. At present, one program for designing three-dimensional finocyl grains has been developed. The program is modular, and calculations are performed step by step allowing parametric studies. The use of this program in a threedimensional finocyl grain has demonstrated that preliminary design is available within one day on a microcomputer PC-286/386 and is performed with

Original languageEnglish
Pages (from-to)53-59
Number of pages7
JournalTuijin Jishu/Journal of Propulsion Technology
Volume56
Issue number2
StatePublished - Apr 1991

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