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本文以实验为基础,研究了双石—2火药在某高速旋转火箭发动机中的侵蚀燃烧现象、规律和特点.文中扼要地介绍了首次设计实现的高速旋转固体火箭发动机的中止燃烧实验的设备、方法;给出了有关的实验现象、结果和侵蚀函数(?)(k)的经验公式;分析讨论了高速旋转火箭发动机中侵蚀燃烧的特点等有关问题. 本文可供火箭、导弹、字航领域内,从事高速旋转固体火箭发动机的设计研究人员、从事固体推进剂及其燃烧机理的研究人员参考;也可作为弹丸专业内从事增程弹、底部排气弹的设计研究人员的参考。
In this paper, based on the experiment, the erosive combustion phenomenon, regularity and characteristics of the double stone-2 gunpowder in a high-speed rotating rocket motor are briefly introduced.The equipment and method of the first-designed high-speed rotating solid rocket motor aborting combustion experiment The empirical formulas of the experimental phenomena, the results and the erosion function (?) (K) are given, and the characteristics of the erosion combustion in the high-speed rotating rocket engine are analyzed and discussed.This paper can be used in the field of rockets, missiles and word- , Engaged in high-speed rotating solid rocket engine design and research personnel engaged in solid propellants and combustion mechanism of the researchers reference; also can be used as projectile professionals in extended range bombs, bottom exhaust bomber design researchers reference.