SOLID PROPELLANT GAS GENERATOR UNSTALLS AIRFOIL

被引:0
|
作者
MAAS, MA
机构
关键词
D O I
暂无
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
引用
收藏
页码:54 / +
页数:1
相关论文
共 50 条
  • [21] Optimum characteristic length of gas generator for liquid propellant rocket engine
    Khan, Taj Wali
    Qamar, Ihtzaz
    [J]. ACTA ASTRONAUTICA, 2020, 176 : 1 - 12
  • [22] On the effect of filters for the design of solid propellant gas generators
    Hong, Moongeun
    Lee, Soo Yong
    [J]. EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2008, 32 (06) : 1248 - 1254
  • [23] Preliminary analysis on properties of solid cool gas propellant
    School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing
    210094, China
    不详
    100080, China
    [J]. Tuijin Jishu, 1 (181-187):
  • [24] Chemical formulation of solid propellant for specific gas generators
    Engelen, K
    Lefebvre, MH
    De Ruyck, J
    [J]. TWENTY-FOURTH INTERNATIONAL PYROTECHNICS SEMINAR, 1998, : 203 - 216
  • [25] Powerful Pulsed Magnetohydrodynamic Generator Fueled by a Solid (Powder) Propellant of a New Generation
    Afonin, A. G.
    Butov, V. G.
    Panchenko, V. P.
    Sinyaev, S. V.
    Solonenko, V. A.
    Shvetsov, G. A.
    Yakushev, A. A.
    [J]. JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS, 2018, 59 (06) : 1024 - 1035
  • [26] Powerful Pulsed Magnetohydrodynamic Generator Fueled by a Solid (Powder) Propellant of a New Generation
    A. G. Afonin
    V. G. Butov
    V. P. Panchenko
    S. V. Sinyaev
    V. A. Solonenko
    G. A. Shvetsov
    A. A. Yakushev
    [J]. Journal of Applied Mechanics and Technical Physics, 2018, 59 : 1024 - 1035
  • [27] Solid-propellant gas generators with a gas flow rate stabilization system
    S. A. Rashkovskii
    Yu. M. Milekhin
    A. V. Fedorychev
    [J]. Doklady Chemistry, 2015, 463 : 189 - 193
  • [28] Solid-propellant gas generators with a gas flow rate stabilization system
    Rashkovskii, S. A.
    Milekhin, Yu M.
    Fedorychev, A. V.
    [J]. DOKLADY CHEMISTRY, 2015, 463 : 189 - 193
  • [29] Combustion of Solid‐Propellant Charges with Highly Progressive Gas Release
    A. M. Lipanov
    [J]. Combustion, Explosion and Shock Waves, 2001, 37 : 550 - 557
  • [30] CALCULATED VISCOSITY OF A SOLID PROPELLANT ROCKET EXHAUST GAS MIXTURE
    GIN, W
    [J]. JET PROPULSION, 1958, 28 (02): : 127 - 128