Research progress of CMC used in rocket motor nozzle and nozzle throat

被引：0
|
作者：
Ning, Wei [1 ]
Jia, De-Chang [1 ]
Yu, Da-Ren [2 ]
机构：
[1] Institute for Advance Ceramics, Harbin Institute of Technology, Harbin 150001, China
[2] Laboratory of Plasma Propulsion Technology, Harbin Institute of Technology, Harbin 150001, China
来源：
Cailiao Kexue yu Gongyi/Material Science and Technology | 2009年 / 17卷 / 03期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：355 / 359
相关论文
共 50 条
  • [1] Progress on Ablation of Nozzle Throat Inserts in Solid Rocket Motors
    Z. T. Zhou
    T. Y. Cao
    Y. Q. Li
    L. Ji
    Fluid Dynamics, 2025, 60 (2)
  • [2] Rocket nozzle throat technology advances
    Rosenberg, B
    AVIATION WEEK & SPACE TECHNOLOGY, 2003, 158 (24): : 199 - 199
  • [3] Development of phased array inspection system for graphite nozzle throat of solid rocket motor
    Koshirae, M
    Kitami, K
    Shiwa, M
    Sato, A
    Sato, E
    SPACE ACTIVITIES AND COOPERATION CONTRIBUTING TO ALL PACIFIC BASIN COUNTRIES, 2004, 117 : 675 - 683
  • [4] The fracture toughness of several rocket nozzle throat materials
    Ran, HX
    Cui, H
    Hao, ZB
    Li, RZ
    Zhou, SJ
    Zhang, Y
    Su, JM
    NEW CARBON MATERIALS, 2002, 17 (01) : 30 - 35
  • [5] Investigation of Carbon–Carbon Nozzle Throat Erosion in a Solid Rocket Motor Under Acceleration Conditions
    Liwu Wang
    Weiping Tian
    Linquan Chen
    Yunqiang Guo
    International Journal of Aeronautical and Space Sciences, 2021, 22 : 42 - 51
  • [6] CAD system of solid rocket motor nozzle
    Xu, Xu
    Yang, Li
    Zhang, Zhenpeng
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 1996, 11 (04): : 373 - 376
  • [7] Thermal stress analysis of a solid rocket motor nozzle throat insert using finite element method
    Mehta, RC
    Suresh, K
    Iyer, RN
    INDIAN JOURNAL OF ENGINEERING AND MATERIALS SCIENCES, 1998, 5 (05) : 271 - 277
  • [8] Investigation of Carbon-Carbon Nozzle Throat Erosion in a Solid Rocket Motor Under Acceleration Conditions
    Wang Liwu
    Tian Weiping
    Chen Linquan
    Guo Yunqiang
    INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2021, 22 (01) : 42 - 51
  • [9] Analysis on faults in the nozzle throat insert of a pulse motor
    Xiang, Sheng-Hai
    Zhang, Ping
    Li, Shi-Peng
    Fang, Shu-Zhou
    Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology, 2006, 26 (05): : 417 - 420
  • [10] Numerical simulation of the dynamic thermostructural response of a composite rocket nozzle throat
    Morozov, E. V.
    de la Beaujardiere, J. F. P. Pitot
    COMPOSITE STRUCTURES, 2009, 91 (04) : 412 - 420
12345