Abstract
The characteristic burning rate (u)-pressure (p) curves of ultrahigh burning rate propellant (UHBRP) were analyzed theoretically. A technological method to reduce the apparent burning rate pressure exponent of UHBRP was used in preparation of UHBRP pellets. A large volume closed bomb was used to measure the burning rates of the UHBRP samples. The u-p curves of UHBRP of density gradient show the plateau combustion characteristics.
| Original language | English |
|---|---|
| Pages (from-to) | 422-425 |
| Number of pages | 4 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 22 |
| Issue number | 5 |
| Publication status | Published - Oct 2001 |
Keywords
- Mesa-burning propellant
- Pressure exponent
- Propellant combustion
- Superhigh burning rate propellant