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Theoretical and experimental investigations of working processes in a triple vortex combustor with spatial arc have been conducted. Selected concept of portable triple vortex plasma assisted combustor can provide higher performance, wider turn down ratios, more efficient propellants utilization, decrease combustor and engine weight, demonstrate potential fuel flexibility, satisfy major gravimetric and volumetric density requirements. Obtained results and recommendations can be used for triple vortex combustor operation modes and geometry optimization, prospective combustors for propulsion and power generation design and engineering.

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