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
  • [21] Calculation of pressure in a solid-propellant rocket motor with the use of a real dependence of the solid propellant burning rate on pressure
    A. M. Lipanov
    Combustion, Explosion, and Shock Waves, 2017, 53 : 569 - 573
  • [22] Measurement of hybrid rocket solid fuel regression rate for a slab burner using deep learning
    Surina, Gabriel, III
    Georgalis, Georgios
    Aphale, Siddhant S.
    Patra, Abani
    DesJardin, Paul E.
    ACTA ASTRONAUTICA, 2022, 190 : 160 - 175
  • [23] Regression Rate Studies of Hybrid Rocket Fuel on a Lab Scale Rocket Motor
    Pal, Yash
    Kumar, V. Ravi
    2015 INTERNATIONAL CONFERENCE ON ROBOTICS, AUTOMATION, CONTROL AND EMBEDDED SYSTEMS (RACE), 2015,
  • [24] FRACTURE OF SOLID ROCKET PROPELLANT GRAINS
    RAO, BN
    ENGINEERING FRACTURE MECHANICS, 1992, 43 (03) : 455 - 459
  • [25] Adhesion in solid propellant rocket motors
    Grythe, Kai Frode
    Hansen, Finn Knut
    Olsen, Torbjorn
    JOURNAL OF ADHESION, 2007, 83 (1-3): : 223 - 254
  • [26] Application of magnalium to solid rocket propellant
    Habu, Hiroto
    Keikinzoku/Journal of Japan Institute of Light Metals, 2008, 58 (04): : 162 - 166
  • [27] Adhesion in solid propellant rocket motors
    Grythe, Kai Frode
    Hansen, Finn Knut
    Olsen, Torbjørn
    Journal of Adhesion, 2007, 83 (03): : 223 - 254
  • [28] A novel kind of solid rocket propellant
    Lo, RE
    AEROSPACE SCIENCE AND TECHNOLOGY, 1998, 2 (06): : 359 - 367
  • [29] Predicting Hybrid Propellant Regression Rate Using Response Surfaces
    Frederick, Robert A., Jr.
    Whitehead, J. Joshua
    JOURNAL OF PROPULSION AND POWER, 2009, 25 (03) : 815 - 818
  • [30] VORTICES IN SOLID PROPELLANT ROCKET MOTORS
    SWITHENBANK, J
    SOTTER, G
    AIAA JOURNAL, 1963, 1 (07) : 1682 - 1684
12345