Abstract
A specifically designed closed vessel test which permits to observe the two combustion stages of a deterred propellant is ^ proposed. Using the experimental derivative pressure history, the deterrent impregnation depth is calculated. This impregnation depth is then compared with values obtained by IR microscopy analyses and satisfactory agreement is achieved.
| Original language | English |
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| Pages | 151-155 |
| Number of pages | 5 |
| Publication status | Published - 2003 |
| Event | Proceedings of the 2003 International Autumn Seminar on Propellants, Explosives and Pyrotechnics (2003 IASPEP) - Theory and Practice of Energetic Materials - Guilin, China Duration: 15 Oct 2003 → 18 Oct 2003 |
Conference
| Conference | Proceedings of the 2003 International Autumn Seminar on Propellants, Explosives and Pyrotechnics (2003 IASPEP) - Theory and Practice of Energetic Materials |
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| Country/Territory | China |
| City | Guilin |
| Period | 15/10/03 → 18/10/03 |
Keywords
- IR microscopy analyses
- Impregnation depth
- Propellant