Autor: |
Gusev, E. V., Zagovorchev, V. A., Pronina, P. F., Rodchenko, V. V., Sadretdinova, E. R. |
Zdroj: |
Russian Aeronautics; Mar2024, Vol. 67 Issue 1, p151-160, 10p |
Abstrakt: |
The mechanism of erosive combustion of gunpowder and its consideration in solid propellant rocket engines are analyzed. The issues of the influence of erosive combustion of a solid fuel on changes in the thrust of a jet penetrator engine are considered. A mathematical model is presented for calculating changes in parameters of the intra-chamber process over time, taking into account their changes along the length of the charge for an engine with a freely inserted tubular charge. The obtained calculation results confirm the significant influence of the charge temperature on the intra-ballistic parameters of the penetrator. [ABSTRACT FROM AUTHOR] |
Databáze: |
Complementary Index |
Externí odkaz: |
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