Effects of control flow parameters on vortex valve SRM thrust modulation

被引:0
|
作者
Wei, Xiang-Geng [1 ]
He, Guo-Qiang [1 ]
Li, Jiang [1 ]
Chen, Jian [1 ]
Yu, Xiao-Jing [1 ]
机构
[1] National Key Lab. of Combustion Flow and Thermo-Structure, Northwestern Polytechnical Univ., Xi'an 710072, China
来源
关键词
Control flows - Mass flow rate - Modulation ratio - Solid propellant rocket motor - Thrust modulation^+ - Vortex valves;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
页码:571 / 575
相关论文
共 50 条
  • [1] Effects of vortex valve geometry parameters on SRM thrust modulation
    Coll. of Astronautics, Northwestern Polytechnical Univ., Xi'an 710072, China
    Tuijin Jishu, 2007, 4 (352-355):
  • [2] Calculating effects of relevant parameters on vortex valve control of variable thrust SRM
    Yu, Xiaojing
    He, Guoqiang
    Li, Jiang
    Liu, Yang
    Wei, Xianggeng
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2009, 27 (02): : 178 - 183
  • [3] COLD FLOW EVALUATION OF PARAMETERS INFLUENCING THRUST MODULATION BY A FLUIDIC VORTEX VALVE
    GREENBERG, I
    WOLFF, H
    ISRAEL JOURNAL OF TECHNOLOGY, 1975, 13 (1-2): : 73 - 81
  • [4] Study on the vortex-valve for the thrust random modulation of solid rocket motor (SRM)
    National Univ of Defense Technology, Changsha, China
    Tuijin Jishu, 5 (34-39):
  • [5] Variable control flow supply angle regulation scheme of vortex valve solid rocket motor thrust modulation
    Wei X.
    Li J.
    Chen J.
    Hou L.
    1600, Beijing University of Aeronautics and Astronautics (BUAA) (32): : 2737 - 2742
  • [6] THRUST MODULATION OF SOLID-PROPELLANT ROCKETS BY A FLUIDIC VORTEX VALVE WITH SECONDARY COMBUSTION
    NATAN, B
    GANY, A
    WOLFF, H
    ACTA ASTRONAUTICA, 1982, 9 (12) : 703 - 711
  • [7] Effects of control parameters on SRM performance: A parametric search
    Bizkevelci, E.
    Ertan, H. B.
    Leblebicioglu, K.
    INTERNATIONAL AEGEAN CONFERENCE ON ELECTRICAL MACHINES AND POWER ELECTRONICS & ELECTROMOTION, PROCEEDINGS, 2007, : 276 - +
  • [8] A VORTEX VALVE FOR FLOW MODULATION OF 5500 DEGREES F GAS
    BLATTER, A
    KERANEN, TW
    JOURNAL OF SPACECRAFT AND ROCKETS, 1970, 7 (02) : 169 - &
  • [9] Analysis of control flow valve compensated thrust bearing considering thrust pad flexibility
    Kumar, Vivek
    Sharma, Satish C.
    Narwat, Kuldeep
    JURNAL TRIBOLOGI, 2020, 25 : 45 - 58
  • [10] Influence of Structural Parameters on the Performance of Vortex Valve Variable-Thrust Solid Rocket Motor
    Wei, Xianggeng
    Li, Jiang
    He, Guoqiang
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2017, 34 (01) : 1 - 9