Discrimination for ablative control mechanism in solid-propellant rocket nozzle

DOI10.1007/S11431-009-0274-2zbMath1178.93103OpenAlexW1995280634MaRDI QIDQ1047414

GuiQing Jiang, Xiaoliang Xu, Haiming Huang

Publication date: 4 January 2010

Published in: Science in China. Series E (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-009-0274-2

zbMATH Keywords

nozzleablationactivation energycontrol mechanismfrequency factor

Mathematics Subject Classification ID

Application models in control theory (93C95) Chemical kinetics in thermodynamics and heat transfer (80A30)

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