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 language | English |
|---|---|
| Pages (from-to) | 76-79 |
| Number of pages | 4 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 26 |
| Issue number | 1 |
| State | Published - Feb 2005 |
Keywords
- Detonation wave
- Experimentation
- Ignition
- Ignition system
- Liquid propellant rocket engine
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