Results 11 to 20 of about 11,282 (264)
Сучасні інформаційні системи, 2022 The problem of choosing the values of the variable parameters of the digital stabilizer of the cosmic stage of a carrier rocket with a liquid-propellant jet engine and an onboard digital computer in the stabilization loop, which ensures stable movement ...
Eugene Aleksandrov +3 more
doaj +3 more sources
Evaluation of the high-frequency oscillation parameters of a liquid-propellant rocket engine with an annular combustion chamber [PDF]
, 2021 The high-frequency instability (HF instability) of a liquid-propellant rocket engine (LPRE) during static firing tests is often accompanied by a significant increase in dynamic loads on the combustion chamber structure, often leading to the chamber ...
O. Nikolayev +3 more
semanticscholar +2 more sources
Concept and Key Technology Analysis of Electric Pump-Fed Liquid Propellant Rocket Engine
, 2021 Electric pump-fed liquid propellant rocket engine is an engine that uses electric pumps for propellant supply and cooling cycle. The engine breaks through the traditional pressurization mode of using inert gas to squeeze the propellant or gas-driven ...
Yang Liu +4 more
semanticscholar +2 more sources
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроениеThe paper presents the results of simulation of spray and combustion processes in the liquid-propellant rocket engine chamber using the z77 reduced kinetic mechanism of chemical reactions and a hybrid method for determining spray parameters of a swirl ...
M. N. Senchev +4 more
doaj +3 more sources
Off-Design Combustion in Liquid-Propellant Rocket Engine with High-Frequency Instability
Transactions of the Japan Society for Aeronautical and Space Sciences, 2019 High-frequency combustion instability is one of the traditional problems of liquid-propellant rocket engines. It damages and melts the engines instantaneously.
T. Kanda
semanticscholar +3 more sources
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2022 Some data on the knowledge base to support the development of low-thrust liquid-propellant rocket engines using computer technologies are presented. The structure of the base is proposed on the basis of characteristic features of engines, including the ...
V. V. Ryzhkov
doaj +3 more sources
Analysis of properties of inertia regulator of thrust control system of liquid rocket engine [PDF]
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", 2021 The quality of the flight task of a space rocket system is determined among other things by the accuracy of maintaining and regulating the thrust of the rocket engine.
M. M. Dron, A. B. Yakovlev
doaj +1 more source
Investigation of a Radial Turbines Compatibility for Small Rocket Engine [PDF]
E3S Web of Conferences, 2020 In the radial turbine preliminary design for an expander rocket engine, a comparison was made with axial turbine used in Pratt & Whitney RL10 engine. One of the primary requirements of a liquid propellant rocket engine is the generation of a high thrust,
Leto Angelo
doaj +1 more source
Reduction of the Pressurization System Final Mass for a Modern Rocket Launcher [PDF]
Journal of Aerospace Technology and Management, 2022 The work focuses on optimizing the pressurization system’s operating performance for a fuel tank of a turbo-pumped liquid propellant rocket engine. This system is the most complex and expensive in a medium-size launch vehicle, after the engine.
Yurii Mitikov, Olexiy Shynkarenko
doaj +3 more sources
Combustion Instabilities and its Control Techniques for Liquid Propellant Rocket Engine
International Journal of Vehicle Structures and Systems, 2023 It is a great challenge for us to understand and to predict the concept of liquid propellant rocket engines combustion instability due to high complex turbulent combustion process.
V. Siva, R. Sivakumar, L. Dinesh Prasaad
semanticscholar +1 more source