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Preliminary experimental investigation on detonation wave ignition technique

  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

To investigate the primary characteristic of detonation wave ignition technique, the experimental system of hydrogen/oxygen detonation wave ignition was designed. Experiments were executed on the condition of pressure 0.1-0.5 MPa and mixture ratio 1.6-9.4 at common temperature. Investigation was made on spreading characteristic of detonation wave in a tube and multi-run reduplication characteristic of detonation wave ignition technique. Results show that pressure above 1 MPa and temperature over 1300°C could be produced from lower gas pressure by detonation wave ignition technique, and the multi-run time difference is less than 0.3 ms.

Original languageEnglish
Pages (from-to)76-79
Number of pages4
JournalTuijin Jishu/Journal of Propulsion Technology
Volume26
Issue number1
StatePublished - Feb 2005

Keywords

  • Detonation wave
  • Experimentation
  • Ignition
  • Ignition system
  • Liquid propellant rocket engine

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