Numerical Study on Response Characteristics of Solid Rocket Pintle Motor
Pintle technology is currently a versatile technology used in a solid rocket motor (SRM) to control the desired thrust by changing the nozzle throat area, while effectively controlling the chamber pressure at the same time. The sudden movement of the pintle can induce rapid changes in the flow field...
| 主要な著者: | , , |
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| フォーマット: | 論文 |
| 言語: | English |
| 出版事項: |
Instituto de Aeronáutica e Espaço (IAE)
2019-08-01
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| シリーズ: | Journal of Aerospace Technology and Management |
| 主題: | |
| オンライン･アクセス: | http://www.scielo.br/pdf/jatm/v11/2175-9146-jatm-11-e3419.pdf |