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This article is cited in 11 scientific papers (total in 11 papers)
Experimental study of thrust performance of a hybrid rocket motor with various methods of oxidizer injection
A. V. Potapkina, T.-S. Leeb a Institute of Theoretical and Applied Mechanics,Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
b Aerospace Science and Technology Research Center (ASTRC), National Cheng Kung University, Tainan, Taiwan. R.O.C.
Abstract:
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 C$_4$H$_6$) 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.
Keywords:
test bench, hybrid rocket motor, solid fuel, swirled oxidizer flow, thrust performance.
Received: 29.12.2002 Accepted: 03.12.2003
Citation:
A. V. Potapkin, T.-S. Lee, “Experimental study of thrust performance of a hybrid rocket motor with various methods of oxidizer injection”, Fizika Goreniya i Vzryva, 40:4 (2004), 15–22; Combustion, Explosion and Shock Waves, 40:4 (2004), 386–392
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https://www.mathnet.ru/eng/fgv1787 https://www.mathnet.ru/eng/fgv/v40/i4/p15
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