REGRESSION RATE OF SOLID PROPELLANT IN A HYBRID ROCKET

被引:0
|
作者
LIEBERHERR, JF
机构
来源
RECHERCHE AEROSPATIALE | 1966年 / 114期
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:31 / +
页数:1
相关论文
共 50 条
  • [31] Stabilization of a solid propellant rocket instability
    Boskovic, DM
    Krstic, M
    PROCEEDINGS OF THE 40TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-5, 2001, : 4483 - 4488
  • [32] Coupled simulation of fluid flow and propellant burning surface regression in a solid rocket motor
    Li, Qiang
    He, Guo-qiang
    Liu, Pei-jin
    Li, Jiang
    COMPUTERS & FLUIDS, 2014, 93 : 146 - 152
  • [33] Consistent definitions for burning rate measurements in solid-propellant rocket motors
    Hessler, R.O.
    Glick, R.L.
    Fizika Goreniya i Vzryva, 2000, 36 (01): : 83 - 106
  • [34] Correlation of Hybrid Rocket Propellant Regression Measurements with Enthalpy-Balance Model Predictions
    Eilers, Shannon D.
    Whitmore, Stephen A.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2008, 45 (05) : 1010 - 1020
  • [35] Geometric effects of fuel regression rate in hybrid rocket motors
    CAI Guo Biao
    ZHANG Yuan Jun
    WANG Peng Fei
    HUI Tian
    ZHAO Sheng
    YU Nan Jia
    Science China(Technological Sciences), 2016, (05) : 807 - 813
  • [36] Scale effect of fuel regression rate in hybrid rocket motor
    Cai, Guobiao
    Zeng, Peng
    Li, Xintian
    Tian, Hui
    Yu, Nanjia
    AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 24 (01) : 141 - 146
  • [37] Geometric effects of fuel regression rate in hybrid rocket motors
    Cai GuoBiao
    Zhang YuanJun
    Wang PengFei
    Hui Tian
    Zhao Sheng
    Yu NanJia
    SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 59 (05) : 807 - 813
  • [38] Geometric effects of fuel regression rate in hybrid rocket motors
    CAI Guo Biao
    ZHANG Yuan Jun
    WANG Peng Fei
    HUI Tian
    ZHAO Sheng
    YU Nan Jia
    Science China(Technological Sciences), 2016, 59 (05) : 807 - 813
  • [39] Internal Flow Dynamics and Regression Rate in Hybrid Rocket Combustion
    Lee, Changjin
    INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2012, 13 (04) : 507 - 514
  • [40] Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines
    Pastrone, Dario
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2012, 2012