Model-Based Robust Transient Control of Reusable Liquid-Propellant Rocket Engines
Sign Up to like & getrecommendations! Published in 2021 at "IEEE Transactions on Aerospace and Electronic Systems"
DOI: 10.1109/taes.2020.3010668
Abstract: Reusable liquid-propellant rocket engines (LPREs) imply more demanding robustness requirements than expendable ones due to their extended capabilities. Therefore, the goal of this article was to develop a control loop adapted to all the operating… read more here.
Keywords: propellant rocket; control; reusable liquid; rocket engines ... See more keywords
Design Procedure of a Movable Pintle Injector for Liquid Rocket Engines
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DOI: 10.2514/1.b36301
Abstract: Variable-area injectors are suitable choices for developing throttleable rocket engines because it is difficult to efficiently control thrust when fixed-area injectors are used. A pintle injector is a variable-area injector that can control the mass… read more here.
Keywords: injector; rocket engines; design procedure; pintle injector ... See more keywords
Model for Combustion Instability in Hybrid Rocket Engines Burning Liquefying Fuels
Sign Up to like & getrecommendations! Published in 2023 at "AIAA Journal"
DOI: 10.2514/1.j062730
Abstract: Starting from the data measured in several static firings of two laboratory-scale hybrid rocket engines of different sizes burning gaseous oxygen with either a liquefying fuel or a pyrolyzing polymer, a mechanism for the combustion… read more here.
Keywords: combustion; hybrid rocket; rocket engines; combustion instability ... See more keywords