Design of a solid rocket motor for characterization of spinning

Zaicheng Wang*, Chunlan Jiang, Ming Li

*Corresponding author for this work

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

Abstract

Although the rocket propulsion technologies have been used for several decades, the traditional motor can not meet the special rotating requirement. A kind of spinning solid rocket motor (SSRM) which used as power device of some kinds of dispenser was introduced. This kind of motor has the structure characterization for tangential nozzles. Its design scheme and prediction of interior ballistic performance were discussed. And the main factors should to be considered in design were analyzed comprehensively. In order to research working performance of the SSRM static test was carried out. The calculation and test results indicate that the design can satisfy general requirement of its application normally.

Original languageEnglish
Title of host publicationAdvanced Research on Mechanical Engineering, Industry and Manufacturing Engineering
Pages621-626
Number of pages6
DOIs
Publication statusPublished - 2011
Event2011 International Conference on Mechanical Engineering, Industry and Manufacturing Engineering, MEIME2011 - Beijing, China
Duration: 23 Jul 201124 Jul 2011

Publication series

NameApplied Mechanics and Materials
Volume63-64
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference2011 International Conference on Mechanical Engineering, Industry and Manufacturing Engineering, MEIME2011
Country/TerritoryChina
CityBeijing
Period23/07/1124/07/11

Keywords

  • Performance test
  • Solid rocket
  • Spinning motor

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