Abstract
The ignition mechanism of solid propellants under high pressure waterjet remained unclear, so HTPB solid propellant of different formulas was used under high-pressure waterjet impact research. The results showed that during the process of impact of high-pressure waterjet with solid propellant the temperature of the samples increased significantly, and that the content of propellant components, ammonium perchlorate and ferrocene affected the heating rate significantly.
| Original language | English |
|---|---|
| Pages (from-to) | 189-191 |
| Number of pages | 3 |
| Journal | Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology |
| Volume | 28 |
| Issue number | 3 |
| Publication status | Published - Mar 2008 |
Keywords
- Ammonium perchlorate (AP)
- Ferrocene
- Solid propellant
- Temperature effect
- Waterjet