Study of instantaneous regression rate in hybrid rocket motor

被引：0
|
作者：
Yang, Yu-Xin [1 ]
Hu, Chun-Bo [1 ]
Qin, Fei [1 ]
Cai, Ti-Min [1 ]
机构：
[1] National Key Laboratory of Combustion, Flow and Thermo-Structure, Coll. of Astronautics, Northwestern Polytechnical Univ., Xi'an 710072, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2008年 / 29卷 / 05期
关键词：
Diaphragms;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：533 / 538
相关论文
共 50 条
  • [1] Dynamic characteristics study of regression rate in variable thrust hybrid rocket motor
    Tian, Hui
    Meng, Xiangyu
    Zhu, Hao
    Li, Chengen
    Yu, Ruipeng
    Zhang, Yuanjun
    Cai, Guobiao
    ACTA ASTRONAUTICA, 2022, 193 : 221 - 229
  • [2] 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,
  • [3] 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
  • [4] Regression rate characteristics of hybrid rocket motor with helical grain
    Tian, Hui
    Li, Yuelong
    Li, Chengen
    Sun, Xingliang
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 68 : 90 - 103
  • [5] Models of the fuel surface regression rate in hybrid rocket motor
    Hu, J.-X.
    Xia, Z.-X.
    2001, Journal of Solid Rocket Technology (24):
  • [6] Regression rate modeling of HTPB/paraffin fuels in hybrid rocket motor
    Wang, Yin
    Hu, Song-qi
    Liu, Xue-li
    Liu, Lin-lin
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 121
  • [7] Regression rate of paraffin-based fuels in hybrid rocket motor
    Liu, Lin-lin
    He, Xiang
    Wang, Yin
    Chen, Ze-bin
    Guo, Quan
    AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 107 (107)
  • [8] Regression rate measurement and analysis for solid fuel in hybrid rocket motor
    Sun, De-Chuan
    Zhang, Yan
    Wang, He
    Liu, Shang
    Wang, Liang
    Tuijin Jishu/Journal of Propulsion Technology, 2010, 31 (01): : 74 - 77
  • [9] Effect of chamber structure on fuel regression rate and performance of hybrid rocket motor
    Wang, Peng-Fei
    Rao, Da-Lin
    Tian, Hui
    Cai, Guo-Biao
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2013, 28 (08): : 1914 - 1920
  • [10] Transient simulation of regression rate on thrust regulation process in hybrid rocket motor
    Tian Hui
    Li Yijie
    Zeng Peng
    Chinese Journal of Aeronautics, 2014, 27 (06) : 1343 - 1351
12345