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
  • [21] IMPORTANCE OF CONDENSED-PHASE REACTIONS IN SOLID-PROPELLANT COMBUSTION
    VERNEKER, VRP
    KISHORE, K
    NAIR, MNR
    ASTRONAUTICS & AERONAUTICS, 1976, 14 (06): : B22 - B22
  • [22] Sensitivity analysis and uncertainty quantification on aluminum particle combustion for an upward burning solid rocket propellant
    Griego, Castillo
    Yilmaz, Nadir
    Atmanli, Alpaslan
    FUEL, 2019, 237 : 1177 - 1185
  • [23] MECHANISM OF TRANSPORT OF CONDENSED COMBUSTION PRODUCTS TO THE SURFACE OF A BURNING MAGNESIUM PARTICLE
    FLORKO, AV
    KOZITSKII, SV
    ZOLOTKO, AN
    GOLOVKO, VV
    COMBUSTION EXPLOSION AND SHOCK WAVES, 1983, 19 (06) : 713 - 717
  • [24] Combustion-mode transition of a solid propellant rocket motor by nitrogen gas injection and combustion gas release
    Tanaka, Masafumi
    Yamakami, Masashi
    Sakaguchi, Taku
    Bando, Shogo
    Wada, Ryusuke
    Ito, Takahiro
    Ito, Toshihito
    Kajiya, Yuta
    SCIENCE AND TECHNOLOGY OF ENERGETIC MATERIALS, 2022, 83 (06) : 163 - 168
  • [25] Unsteady flow evolution and combustion dynamics of homogeneous solid propellant in a rocket motor
    Apte, S
    Yang, V
    COMBUSTION AND FLAME, 2002, 131 (1-2) : 110 - 131
  • [26] Numerical Simulation of the Gas Flow of Combustion Products from Ignition in a Solid Rocket Motor Under Conditions of Propellant Creep
    Zhang, Yin
    Sun, Zhensheng
    Hu, Yu
    Zhu, Yujie
    Xia, Xuefeng
    Qu, Huang
    Tian, Bo
    AEROSPACE, 2025, 12 (02)
  • [27] Rocket Engine with Continuous Detonation Combustion of the Natural Gas–Oxygen Propellant System
    S. M. Frolov
    V. S. Aksenov
    V. S. Ivanov
    S. N. Medvedev
    I. O. Shamshin
    N. N. Yakovlev
    I. I. Kostenko
    Doklady Physical Chemistry, 2018, 478 : 31 - 34
  • [28] Condensed combustion products of aluminized propellants. II. evolution of particles with distance from the burning surface
    O. G. Glotov
    Combustion, Explosion and Shock Waves, 2000, 36 : 476 - 487
  • [29] Condensed combustion products of aluminized propellants. II. Evolution of particles with distance from the burning surface
    Glotov, OG
    COMBUSTION EXPLOSION AND SHOCK WAVES, 2000, 36 (04) : 476 - 487
  • [30] 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
    A. V. Rudinskii
    V. I. Lapitskii
    D. A. Yagodnikov
    Combustion, Explosion, and Shock Waves, 2019, 55 : 566 - 573
12345