Abstract
The combustion behavior of aluminium-magnesium based solid fuel-rich propellants was investigated using modified strand burner and high-speed motion analysis system. Ignition property, burning process and the relationship between burning rate, main ingredients and catalyzers were discussed under the oxygen poor condition of the pressure less than 3 MPa. Preliminary combustion process, appearance of burning and flame, and sediment were observed. The ingredients and cause of sediment were analyzed, as well as the influence factors.
| Original language | English |
|---|---|
| Pages (from-to) | 342-345 |
| Number of pages | 4 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 23 |
| Issue number | 4 |
| State | Published - Aug 2002 |
Keywords
- Burning rate
- Burning rate modifier
- Burning rate testing
- Combustion catalyst
- Oxygen-poor fuel-rich propellant