INVESTIGATION OF AN ADDITIONAL OXIDIZER CHARGE EFFECT ON SELECTED OPERATIONAL CHARACTERISTICS OF A SOLID-FUEL ROCKET ENGINE

被引：0
|
作者：
Zyluk, Andrzej [1 ]
Pietraszek, Mariusz [1 ]
机构：
[1] AF Inst Technol, Warsaw, Poland
来源：
JOURNAL OF THEORETICAL AND APPLIED MECHANICS | 2014年 / 52卷 / 01期
关键词：
oxygen balance; rocket engine; aircraft; experimental examination; oxidizer charge;
D O I：
暂无
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The paper has been intended to discuss some issues closely related to the elimination of an extremely disadvantageous phenomenon, i.e. the occurrence of a negative oxygen balance in products of combustion emitted by a solid-fuel rocket engine while launching a missile from the aircraft. Findings of experimental examination of such engines furnished with an additional oxidizer charge have also been presented.
引用
收藏
页码：139 / 149
页数：11
相关论文
共 50 条
  • [31] Experimental investigation of thermal effect on cavitation characteristics in a liquid rocket engine turbopump inducer
    Wang, Chunmin
    Xiang, Le
    Tan, Yonghua
    Chen, Hui
    Xu, Kaifu
    CHINESE JOURNAL OF AERONAUTICS, 2021, 34 (08) : 48 - 57
  • [32] Experimental investigation of thermal effect on cavitation characteristics in a liquid rocket engine turbopump inducer
    Chunmin WANG
    Le XIANG
    Yonghua TAN
    Hui CHEN
    Kaifu XU
    Chinese Journal of Aeronautics , 2021, (08) : 48 - 57
  • [33] Investigation on Flow Features and Combustion Characteristics in a Boron-Based Solid-Ducted Rocket Engine
    Tang, Xiang
    Tian, Xiaotao
    Zhu, Liang
    Wu, Suli
    Huang, Meng
    Li, Weixuan
    ENERGIES, 2025, 18 (03)
  • [34] Effect of metal and metalloid solid-fuel additives on performance and nozzle ablation in a hydroxy-terminated polybutadiene based hybrid rocket motor
    Tian, Hui
    Wang, Zhongshuo
    Guo, Zihao
    Yu, Ruipeng
    Cai, Guobiao
    Zhang, Yuanjun
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 123
  • [35] Effect of fuel and engine operational characteristics on the heat loss from combustion chamber surfaces of SI engines
    Jafari, A
    Hannani, SK
    INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2006, 33 (01) : 122 - 134
  • [36] The decoupled effect of oxidizer mass flux and combustion pressure on turbulent combustion characteristics of finite-length solid fuel
    Xia, Hanqing
    Wang, Ningfei
    Pang, Jiantao
    Zhang, Yiming
    Wang, Ran
    Wu, Yi
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 155
  • [37] SEMIEMPIRICAL METHOD FOR CALCULATING THE THRUST CHARACTERISTICS OF A SYSTEM FOR CONTROLLING THE THRUST VECTOR BY GAS INJECTION INTO THE SUPERSONIC PART OF A SOLID-FUEL ROCKET-MOTOR NOZZLE.
    Vinogradov, B.S.
    Naumov, Yu.N.
    Klevanskii, V.M.
    Shaikhutdinov, Z.G.
    Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika), 1981, 24 (03): : 28 - 31
  • [38] Investigation of intake pressure and fuel injection timing effect on performance characteristics of diesel engine
    Anggono, Willyanto
    Ikoma, Wataru
    Chen, Haoyu
    Liu, Zhiyuan
    Ichiyanagi, Mitsuhisa
    Suzuki, Takashi
    Gotama, Gabriel Jeremy
    2019 9TH INTERNATIONAL CONFERENCE ON FUTURE ENVIRONMENT AND ENERGY, 2019, 257
  • [39] Numerical investigation of the influence of crystallization of ultrafine particles of aluminum oxide on energy characteristics of solid-propellant rocket engine
    Dyachenko, N. N.
    Dyachenko, L. I.
    THERMOPHYSICS AND AEROMECHANICS, 2014, 21 (04) : 509 - 513
  • [40] Numerical and experimental investigation of the effect of biodiesel/diesel fuel on combustion characteristics in CI engine
    Temizer, Ilker
    Cihan, Omer
    Eskici, Bunyamin
    FUEL, 2020, 270
12345