The Influence of Flow Regulator Dynamics on the Internal Ballistic Parameters of Multi-Nozzle Solid Propellant Propulsion. Results of Numerical Modeling

The Influence of Flow Regulator Dynamics on the Internal Ballistic Parameters of Multi-Nozzle Solid Propellant Propulsion. Results of Numerical Modeling

The paper presents the mathematical model, numerical algorithm and results of parametric study for the parameters of multi-nozzle solid propellant propulsion supplied with the stepper regulators of mass flow rate.

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Veröffentlicht in:Russian aeronautics 2022, Vol.65 (1), p.180-185
Hauptverfasser: Bitkin, S. A., Elyukin, N. N., Korepanov, M. A., Karpov, A. I.
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft and Rocket Engine Theory
Algorithms
Automotive Engineering
Engineering
Flow regulators
Mass flow rate
Mathematical models
Nozzles
Numerical analysis
Parameters
Solid propellants
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Beschreibung
Zusammenfassung:The paper presents the mathematical model, numerical algorithm and results of parametric study for the parameters of multi-nozzle solid propellant propulsion supplied with the stepper regulators of mass flow rate.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799822010202