Experimental investigation on ignition of H2O2/HTPB hybrid rocket engine

被引：0
|
作者：
Song, Zhi-Bing [1 ]
Wang, Zhen-Guo [1 ]
Zhang, Wei [1 ]
Xia, Zhi-Xun [1 ]
Hu, Jian-Xin [1 ]
机构：
[1] College of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China
来源：
Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology | 2008年 / 30卷 / 01期
关键词：
5;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：28 / 31
相关论文
共 50 条
  • [1] Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor
    Li, Meng-Che
    Chang, Chih-Shin
    Wei, Shih-Sin
    Wu, Jong-Shinn
    JOURNAL OF PROPULSION AND POWER, 2022, 39 (01) : 63 - 70
  • [2] Two-phase flow numerical calculation of H2O2/HTPB hybrid rocket engine with diaphragm in grain
    Wang, Peng-Fei
    Tian, Hui
    Yu, Nan-Jia
    Cai, Guo-Biao
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2013, 28 (11): : 2621 - 2626
  • [3] Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels
    Stella, Manuel
    Zeni, Lucia
    Nichelini, Luca
    Bellomo, Nicolas
    Pavarin, Daniele
    Migliorino, Mario Tindaro
    Fabiani, Marco
    Bianchi, Daniele
    Nasuti, Francesco
    Paravan, Christian
    Galfetti, Luciano
    Cretella, Attilio
    Pellegrini, Rocco Carmine
    Cavallini, Enrico
    Barato, Francesco
    APPLIED SCIENCES-BASEL, 2024, 14 (13):
  • [4] Orthogonal optimal design of solid fuel formulation for H2O2/HTPB hybrid rocket motor
    Zeng, Peng
    Tian, Hui
    Li, Xin-Tian
    Cai, Guo-Biao
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2013, 28 (05): : 1180 - 1186
  • [5] Experimental and numerical investigation of swirling H2O2 and polypropylene hybrid rocket motor with regenerative cooling
    Li, M-C
    Wei, S-S
    Hung, C-H
    Wu, J-S
    ACTA ASTRONAUTICA, 2022, 190 : 283 - 298
  • [6] Experimental investigation on catalytic ignition of N2O hybrid rocket motor
    Space Centre, Tsinghua Univ., Beijing 100084, China
    Tuijin Jishu, 2007, 1 (1-3+85):
  • [7] Development of H2O2 Based Mixed Hybrid Rocket
    Marothiya, Gaurav
    Ramakrishna, P. A.
    Saravanan, N.
    Kumar Solasa, Praveen
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2021, 46 (11) : 1687 - 1695
  • [8] Experimental research of regression rate of N2O and metalized HTPB hybrid rocket motor
    Tian, Hui
    Wu, Jun-Feng
    Yu, Nan-Jia
    Li, Jun-Hai
    Cai, Guo-Biao
    Tuijin Jishu/Journal of Propulsion Technology, 2014, 35 (03): : 413 - 421
  • [9] Experimental Study of the Swirling Oxidizer Flow in HTPB/N2O Hybrid Rocket Motor
    Heydari, Mohammad Mahdi
    Massoom, Nooredin Ghadiri
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2017, 2017
  • [10] Experimental study of fuel regression rate in an HTPB/N2O hybrid rocket motor
    Rezaei, H.
    Soltani, M. R.
    Mohammadi, A. R.
    SCIENTIA IRANICA, 2018, 25 (01) : 253 - 265
12345