Two-zone model for combustion of a composite solid propellant with a coolant
| Autor: | G. B. Manelis, V. A. Strunin, S. V. Gunin, A. N. Klyuchnikov, A. V. Fedorychev, Yu. M. Milekhin |
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| Rok vydání: | 2010 |
| Předmět: |
Propellant
Materials science Component (thermodynamics) General Chemical Engineering Composite number General Physics and Astronomy Energy Engineering and Power Technology Thermodynamics General Chemistry Combustion Kinetic energy Coolant Burn rate (chemistry) Fuel Technology Sensitivity (control systems) |
| Zdroj: | Combustion, Explosion, and Shock Waves. 46:315-324 |
| ISSN: | 1573-8345 0010-5082 |
| DOI: | 10.1007/s10573-010-0044-2 |
| Popis: | A mathematical model for combustion of a propellant with a coolant taking into account the two-zone structure of the combustion front due to condensed- and gas-phase reactions was developed and examined. Formulas for the burning rate, reaction-zone temperature, and burning-rate sensitivity to internal and external parameters of the system were derived in analytical form. The burning rate was examined numerically as a function of pressure, the characteristic size of the system, component content, and thermodynamic and kinetic parameters. Recommendations are given on methods of obtaining particular ballistic properties by varying the initial parameters of the system. |
| Databáze: | OpenAIRE |
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