Experimental investigation of the effect of nozzle throat diameter on the performance of a hybrid rocket motor with swirling injection of high-concentration hydrogen peroxide - Concepedia

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Experimental investigation of the effect of nozzle throat diameter on the performance of a hybrid rocket motor with swirling injection of high-concentration hydrogen peroxide

27

Citations

9

References

2019

Year

S.-S. Wei, Meng-Chieh Lee, Y. H. Chien, T.H. Chou, Jong‐Shinn Wu

Acta Astronautica

EngineeringExperimental InvestigationMechanical EngineeringRocket EngineIn-cylinder FlowNozzle Throat DiameterAerodynamicsAerospace Propulsion SystemsPropulsionHybrid Rocket Motor

References

	Year	Citations

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