Verification of Model of Calculation of Intra-Chamber Parameters In Hybrid Solid-Propellant Rocket Engines

On the basis of obtained analytical estimate of characteristics of hybrid solid-propellant rocket engine verification of earlier developed physical and mathematical model of processes in a hybrid solid-propellant rocket engine for quasi-steady-state flow regime was performed. Comparative analysis of...

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Bibliographic Details
Published in:MATEC Web of Conferences Vol. 72; p. 1135
Main Authors: Zhukov, Ilya S., Borisov, Boris V., Bondarchuk, Sergey S., Zhukov, Alexander S.
Format: Journal Article Conference Proceeding
Language:English
Published: Les Ulis EDP Sciences 01-01-2016
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Summary:On the basis of obtained analytical estimate of characteristics of hybrid solid-propellant rocket engine verification of earlier developed physical and mathematical model of processes in a hybrid solid-propellant rocket engine for quasi-steady-state flow regime was performed. Comparative analysis of calculated and analytical data indicated satisfactory comparability of simulation results.
ISSN:2261-236X
2274-7214
2261-236X
DOI:10.1051/matecconf/20167201135