The dynamics of intrachamber processes in a type of solid propellant rocket engine under consideration is investigated in order to optimize its parameters. The conjugate statement of the problem at the level of setting up a computational experiment is formulated. The results of numerical calculations are presented, which revealed an anomalous feature of the rocket engine firing process.
Anomalous Features of Dynamics of Intrachamber Processes in a Low-Thrust Solid Propellant Rocket Engine with a Multi-Grain Propellant Charge
Russ. Aeronaut.
Russian Aeronautics ; 64 , 4 ; 711-720
01.10.2021
10 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Thrust Variation of a Gaseous Propellant Rocket Engine
NTIS | 1967
|TECHNICAL NOTES - Thrust Termination Dynamics of Solid Propellant Rocket Motors
Online Contents | 2007
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