推进技术 ›› 1992, Vol. 13 ›› Issue (3): 28-34.

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固体火箭发动机平均燃速预示

林小树   

  1. 航空航天部41所
  • 发布日期:2021-08-15

PREDICTION OF THE MEAN BURNING RATE IN SOLID ROCKET MOTOR

  1. The 41st Research Institute
  • Published:2021-08-15

摘要: 提出了用推进剂燃烧性能参数预示发动机平均燃速的思想。阐述了燃烧性能和燃烧环境的概念。导出了用推进剂燃烧性能参数预示发动机平均燃速的通用方法,并用试验数据对这一方法进行了验证。

关键词: 固体火箭发动机;燃烧速度;预测

Abstract: It is proposed that the mean burning rate in solid rocket motor can be predicted by using propcllant burning performance paramc-ters,which depend on both propellant and burning environment. A feasible method for prediciting the solid rocket motor mean burning rate is discussed in the paper, and the resales are in agreement with the test data.

Key words: Solid rocket engine;Burning rate;Prediction