Experimental Study of Thrust Performance of a Hybrid Rocket Motor with Various Methods of Oxidizer Injection

被引：0
|
作者：
A. V. Potapkin
T.‐S. Lee
机构：
[1] Russian Academy of Sciences,Institute of Theoretical and Applied Mechanics,Siberian Division
[2] National Cheng Kung University,Aerospace Science and Technology Research Center (ASTRC)
来源：
Combustion, Explosion and Shock Waves | 2004年 / 40卷
关键词：
test bench; hybrid rocket motor; solid fuel; swirled oxidizer flow; thrust performance;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
A test bench and technique for experimental investigation of thrust performance of a hybrid rocket motor are described. A configuration of a rocket motor operating on a solid fuel (polymerized unsaturated hydrocarbon C4H6) and gaseous oxygen is proposed. Measured results for motor thrust are given. It is demonstrated that injection of a swirled oxygen flow into the motor duct increases the thrust performance of this kind of motors.
引用
收藏
页码：386 / 392
页数：6
相关论文
共 50 条
  • [21] Performance of hybrid rocket with various oxidizers
    Chang, Ming Fu
    Hsing, Yue Cheng
    Hangkong Taikong ji Minhang Xuekan/Journal of Aeronautics, Astronautics and Aviation, 2008, 40 A (01): : 35 - 40
  • [22] Experimental and theoretical study on a dual-thrust rocket motor with subsonic intermediate nozzle
    El-Nady, A. M.
    Ahmed, M. Y. M.
    El-Senbawy, M. A.
    Sarhan, A. M.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 232 (10) : 1844 - 1852
  • [23] Experimental study on precise thrust control of hydrogen peroxide and polyethylene hybrid rocket motors
    Tan Guang
    Tian Hui
    Jiang Xianzhu
    Chen Ruikai
    Lu Yudong
    Zhang Yuanjun
    ACTA ASTRONAUTICA, 2022, 196 : 303 - 313
  • [24] PARAMETRIC STUDY OF A HYBRID ROCKET MOTOR
    GANY, A
    MANHEIME.Y
    ISRAEL JOURNAL OF TECHNOLOGY, 1972, 10 (1-2): : 85 - &
  • [25] Experimental Investigation of Dual-Thrust Rocket Motor with Intermediate Nozzle
    El-Nady, A. M.
    Ahmed, M. Y. M.
    El-Senbawy, M. A.
    Sarhan, A. M.
    JOURNAL OF PROPULSION AND POWER, 2017, 33 (05) : 1285 - 1293
  • [26] Experimental Investigation of Combustion in Axial-Injection End-Burning Hybrid Rocket Motor
    Li, Xintian
    Tian, Hui
    Yu, Nanjia
    Cai, Guobiao
    JOURNAL OF PROPULSION AND POWER, 2015, 31 (03) : 930 - 936
  • [27] DEVELOPMENT OF TEST FACILITIES FOR 5 KN-THRUST HYBRID ROCKET ENGINES AND A SWIRLING-OXIDIZER-FLOW-TYPE HYBRID ROCKET ENGINE FOR TECHNOLOGY DEMONSTRATION
    Kitagawa, K.
    Yuasa, S.
    Sakurai, T.
    Hatagaki, S.
    Shiraishi, N.
    Ando, H.
    Yagishita, T.
    Suzuki, N.
    Takayama, A.
    Yui, R.
    Shimada, T.
    INTERNATIONAL JOURNAL OF ENERGETIC MATERIALS AND CHEMICAL PROPULSION, 2016, 15 (06) : 435 - 451
  • [28] Axial-Injection End-Burning Hybrid Rocket Motor Sensitivity Study
    Hitt, Matthew A. A.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2023, 60 (05) : 1664 - 1668
  • [29] Parametric investigation of secondary injection in post-chamber on combustion performance for hybrid rocket motor
    Cai, Guobiao
    Cao, Binbin
    Zhu, Hao
    Tian, Hui
    Ma, Xuan
    ACTA ASTRONAUTICA, 2017, 140 : 427 - 438
  • [30] 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