Study on combustion properties of new high burning rate propellant in solid rocket motor

被引:0
|
作者
National Special Superfine Powder Engineering Research Center, Nanjing University of Science and Technology, Nanjing 210094, China [1 ]
机构
关键词
D O I
暂无
中图分类号
学科分类号
摘要
7
引用
下载
收藏
页码:48 / 51
相关论文
共 50 条
  • [41] Study on optimization of combustion technology in solid propellant air turbo rocket
    Li, J. (lijiang@nwpu.edu.cn), 1600, Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China (36):
  • [42] EFFECTS OF HIGH SPIN ON INTERNAL BALLISTICS OF A SOLID PROPELLANT ROCKET MOTOR
    BRODDNER, S
    ASTRONAUTICA ACTA, 1970, 15 (04): : 191 - &
  • [43] Study on burning rate catalysis of ultra-high burning rate propellant
    Tang, Songqing
    Gong, Hua
    Yan, Sihai
    Miao, Lin
    He, Fumei
    Tang, Dasen
    Liu, Xun'en
    Yang, Rongjie
    Jing, Zhongxing
    Shiyou Daxue Xuebao/Journal of the University of Petroleum China, 1998, 22 (05): : 91 - 94
  • [44] Ballistic project of solid propellant rocket motor
    Konecny, Pavel
    2002, Military Academy Brno
  • [45] Study of flow in combustion chamber of solid rocket motor
    Amano, R. S.
    Xiao, Y.
    TURBULENCE, HEAT AND MASS TRANSFER 6, 2009, : 1107 - 1110
  • [46] Numerical Study on Internal Ballistics Characteristics of a Solid Propellant Rocket Motor
    Rackauskas, Saulius
    Fedaravicius, Algimantas
    Survila, Arvydas
    MECHANIKA, 2019, 25 (03): : 187 - 196
  • [47] COMBUSTION INSTABILITY AND DESIGN OF SOLID PROPELLANT ROCKET MOTORS
    ROBERTS, AK
    BROWNLEE, WG
    JACKSON, F
    CANADIAN AERONAUTICS AND SPACE JOURNAL, 1969, 15 (05): : 202 - &
  • [48] COMBUSTION INSTABILITY AND DESIGN OF SOLID PROPELLANT ROCKET MOTORS
    ROBERTS, AK
    BROWNLEE, WG
    JACKSON, F
    CANADIAN AERONAUTICS AND SPACE JOURNAL, 1970, 16 (01): : 21 - &
  • [49] Measurement system for determining solid rocket propellant burning rate using reflection microwave interferometry
    Bozic, VS
    Blagojevic, DD
    Anicin, BA
    JOURNAL OF PROPULSION AND POWER, 1997, 13 (04) : 457 - 462
  • [50] REGRESSION RATE OF SOLID PROPELLANT IN A HYBRID ROCKET
    LIEBERHERR, JF
    RECHERCHE AEROSPATIALE, 1966, (114): : 31 - +