Verification of Model of Calculation of Intra-Chamber Parameters In Hybrid Solid-Propellant Rocket Engines
1 Tomsk State University, 634050 Tomsk, Russia
2 Tomsk Polytechnic University, 634050 Tomsk, Russia
3 Tomsk State Pedagogical University, 634057 Tomsk, Russia
* Corresponding author: email@example.com
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.
© The Authors, published by EDP Sciences, 2016
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