Investigation into Distinctive Features of Combustion of High-Density Propellants Under the Conditions of a Manometric Bomb

被引：0
|
作者：
Rogaev, K. S. [1 ]
Ishchenko, A. N. [1 ]
D'yachkovskii, A. S. [1 ]
Samorokova, N. M. [1 ]
Stepanov, E. Yu. [1 ]
Chupashev, A. V. [1 ]
机构：
[1] Tomsk State Univ, Natl Res Tomsk State Univ, Autonomous Struct Subdiv Sci Res Inst Appl Math &, 36 Lenin Ave,Bldg 27, Tomsk 634050, Russia
来源：
JOURNAL OF ENGINEERING PHYSICS AND THERMOPHYSICS | 2023年 / 96卷 / 4期
关键词：
manometric bomb; combustion law; model high-density propellant; paste propellant;
D O I：
10.1007/s10891-023-02755-4
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
The combustion of a model high-density propellant (MHP) under the conditions of a closed volume has been investigated. A description is given of the main components and mechanisms of the manometric bomb being used. Procedures are described for determining the laws of propellant combustion in a manometric experiment, and a comparison is made of computational-experimental data. The distinctive features of the formation of an MHP combustion surface in various containers have been identified and described. The dependences of the layer combustion velocity of two model high-density propellants on pressure have been determined.
引用
收藏
页码：928 / 938
页数：11
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