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Verification of model of calculation of intra-chamber parameters in hybrid solid-propellant rocket engines I. S. Zhukov, B. V. Borisov, S. S. Bondarchuk, A. S. Zhukov
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ArticleSubject(s): твердотопливные ракетные двигатели | гибридные ракетные двигатели | квазистационарный режим течения | внутрикамерные процессы | физико-математические моделиGenre/Form: статьи в журналах Online resources: Click here to access online
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MATEC Web of conferences Vol. 72. P. 01135 (1-4)Abstract: 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.
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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.
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