Performance and Regression Rate Characteristics of 5-kN Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine
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DOI: 10.2514/1.b36239
Abstract: Burning tests were carried out for the 5-kN-thrust swirling-oxidizer-flow-type hybrid rocket engine to establish the engine technology and to obtain the fuel regression characteristics. The engine attained stable burning without any combustion oscillation and C*… read more here.
Keywords: swirling oxidizer; engine; regression rate; flow ... See more keywords