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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Published in: | MATEC Web of Conferences Vol. 72; p. 1135 |
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Main Authors: | , , , |
Format: | Journal Article Conference Proceeding |
Language: | English |
Published: |
Les Ulis
EDP Sciences
01-01-2016
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Subjects: | |
Online Access: | Get full text |
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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. |
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ISSN: | 2261-236X 2274-7214 2261-236X |
DOI: | 10.1051/matecconf/20167201135 |