Abstract
The key technique to the investigation of ablation characteristic of the insulators of solid rocket motor with high acceleration is to develop a method to produce high concentration particles stream. A convergent tube experimental method was developed based on the previous principle experiments. A convergent tube test facility was designed to demonstrate this method. Three-dimensional two-phase numerical simulations were carried to compare the particles distributions of this test facility and the solid rocket motor with high acceleration. Numerical results show that high concentration particles distribution in test facility is similar to that in the chamber of rocket motor with 40 g longitudinal and lateral accelerations. Ablation experiments of six kinds of insulator were carried in this convergent tube facility. The experimental results show that a cavity is formed on the surface of insulator due to the erosion of high concentration particles stream. This phenomenon indicates that erosion of particles has a strong influence on the insulator ablation. The location of cavity accords with the location of the highest concentration of particles of numerical results.
| Original language | English |
|---|---|
| Pages (from-to) | 196-198 |
| Number of pages | 3 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 25 |
| Issue number | 3 |
| State | Published - Jun 2004 |
Keywords
- Ablation
- Heat insulation layer
- High acceleration
- Solid propellant rocket motor