Key technique of hybrid rocket motor and its development

Yu Xin Yang, Chun Bo Hu, Guo Qiang He, Ti Min Cai

Research output: Contribution to journalArticlepeer-review

7 Scopus citations

Abstract

Basing the structure and operation process of hybrid rocket motor, both of its advantages and disadvantages were presented. Also, concluding the national and foreign research so far, the key techniques and difficulties were summarized as follows: 1.developing high-energy solid fuel and raising regression rate of the solid fuel; 2.measuring regression rate of solid fuel during operation; 3.studing pyrogenation of different solid fuels; 4.building formulation of solid fuel regression rate; 5. repressing unstable combustion; 6.establishing subscale rule; 7.developing numerical model of hybrid rocket motor operation. All of adopted technique, progress, and future development were concluded.

Original languageEnglish
Pages (from-to)1616-1621
Number of pages6
JournalYuhang Xuebao/Journal of Astronautics
Volume29
Issue number5
StatePublished - Sep 2008

Keywords

  • Hybrid rocket motor
  • Key technique
  • Method
  • Regression rate
  • Unstable combustion

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