Investigation of the rocket motor dimensionless geometric parameters influence on the burning rate of double base propellant
The investigation included experimental and theoretical studies of internal ballistic characteristics with a particular attention to erosive rate burning in function of propellant-motor system geometric parameters. Experimental investigations have been performed of the defined double base propellant...
| 出版年: | Vojnotehnički Glasnik |
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| 主要な著者: | , |
| フォーマット: | 論文 |
| 言語: | 英語 |
| 出版事項: |
University of Defence in Belgrade
2001-01-01
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| 主題: | |
| オンライン･アクセス: | https://scindeks.ceon.rs/article.aspx?artid=0042-84690101053T |
| 要約: | The investigation included experimental and theoretical studies of internal ballistic characteristics with a particular attention to erosive rate burning in function of propellant-motor system geometric parameters. Experimental investigations have been performed of the defined double base propellant. DRG-X, in a test motor specially designed for this purpose. The experimental results of burning rate (basic and erosive) are presented. Corresponding models of burning rates and erosion effects have been derived as well. |
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| ISSN: | 0042-8469 2217-4753 |