Experimental study of evolution of condensed combustion products in gas phase of burning soled rocket propellant

被引：0
|
作者：
Babuk, VA [1 ]
Vassiliev, VA [1 ]
Naslednikov, PA [1 ]
机构：
[1] Balt State Tech Univ, St Petersburg, Russia
来源：
COMBUSTION OF ENERGETIC MATERIALS | 2002年
关键词：
agglomerate; two-phase flow; aluminum; aluminum oxide; solid rocket propellant;
D O I：
暂无
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
In the two-phase flow of a solid propellant rocket motor, condensed combustion products suffer a set of physical and chemical transformations, which constitute the condensed combustion products evolution process. The process of condensed combustion products formation in the surface layer of burning propellants and their evolution in the gas phase determines efficiency of the metal fuel as a component of solid rocket propellant. The objective of this paper is the experimental study of the evolution of condensed combustion products in the gas phase of burning solid rocket propellants.
引用
收藏
页码：412 / 426
页数：3
相关论文
共 50 条
  • [31] Effect of Condensed Phase Particles on the Electromagnetic Field Characteristics of Combustion Products in a Flow Path of a Liquid-Propellant Engine. The Results of Experimental Studies
    Rudinskii, A., V
    Lapitskii, V., I
    Yagodnikov, D. A.
    COMBUSTION EXPLOSION AND SHOCK WAVES, 2019, 55 (05) : 566 - 573
  • [32] CONTRIBUTION OF CONDENSED-PHASE REACTIONS IN COMBUSTION OF SOLID ROCKET FUELS
    KISHORE, K
    PAIVERNEKER, VR
    SUNITHA, MR
    PRASAD, G
    FUEL, 1977, 56 (03) : 347 - 348
  • [33] TEMPERATURE-MEASUREMENT IN GAS-PHASE OF A BURNING PROPELLANT
    ZARKO, VE
    SUKHININ, AI
    KHLEVNOI, SS
    COMBUSTION EXPLOSION AND SHOCK WAVES, 1970, 6 (04) : 487 - 491
  • [34] Experimental Study of the Disperse Composition of Condensed Products of Aluminum‐Particle Combustion in Air
    D. A. Yagodnikov
    E. I. Gusachenko
    Combustion, Explosion and Shock Waves, 2004, 40 : 154 - 162
  • [35] Experimental Study on Rebound Characteristics of Condensed Products in Metal Powder Combustion Device
    Wang Z.-Q.
    Hu C.-B.
    Li M.-Z.
    Hu J.-M.
    Tuijin Jishu/Journal of Propulsion Technology, 2021, 42 (11): : 2538 - 2545
  • [36] SOLID-PROPELLANT BURNING ALONG A TUBE HEATED BY COMBUSTION GAS INFLUX
    CAVENY, LH
    SAWYER, TT
    AIAA JOURNAL, 1967, 5 (11) : 2004 - &
  • [37] Calculation of solid propellant burning rates from condensed-phase decomposition kinetics
    Waesche, R. H. W.
    THEORY AND PRACTICE OF ENERGETIC MATERIALS, VOL VII, 2007, : 656 - 665
  • [38] Calculation of solid propellant burning rates from condensed-phase decomposition kinetics
    2000, Izdatel'stvo SO RAN (36):
  • [39] Collection Method of Condensed Combustion Products of Solid Propellant Based on Constant Quenching Distance
    Gou D.-L.
    Ao W.
    Gao Y.
    Fan Z.-M.
    Liu P.-J.
    Lyu X.
    He G.-Q.
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (04):
  • [40] Effects of Collection and Treatment Methods on Characteristics of Condensed Combustion Products of Aluminized Solid Propellant
    Liu H.
    Liu P.-J.
    Hu S.-Q.
    Ao W.
    Tuijin Jishu/Journal of Propulsion Technology, 2019, 40 (01): : 206 - 214
12345