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
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