Results 51 to 60 of about 190,559 (293)

A Numerical Approach to Optimize the Design of a Pintle Injector for LOX/GCH4 Liquid-Propellant Rocket Engine

open access: yesAerospace, 2023
This study presents an optimal design approach of a pintle injector for a deep throttlable liquid-propellant rocket engine (LPRE). Even though the pintle injector is used in rocket engines, it has become more important since reusable launch vehicles ...
Jihyoung Cha   +2 more
doaj   +1 more source

Reduced Order Modeling Approach to Combustion Instabilities of Liquid Rocket Engines

open access: yesAIAA Journal, 2018
This paper describes one possible approach to a numerical framework for a reduced order tool that aims to simulate combustion instabilities in liquid rocket engines.
M. Gonzalez-Flesca   +5 more
semanticscholar   +1 more source

Intelligent Fault Diagnosis of Liquid Rocket Engine via Interpretable LSTM with Multisensory Data

open access: yesItalian National Conference on Sensors, 2023
Fault diagnosis is essential for high energy systems such as liquid rocket engines (LREs) due to harsh thermal and mechanical working environment.
Xiaoguang Zhang   +3 more
semanticscholar   +1 more source

Modelling Rocket System Performance Parameters

open access: yesAcademy Journal of Science and Engineering, 2022
What distinguishes the rocket system from airbreathing engines is that the rocket carries its own propellants, fuel and oxidants.  The modern rocket was originally developed for ballistic missiles.
Nnorom Achara
doaj  

Analysis of low-thrust liquid rocket engines with a methane air pump unit

open access: yesВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2016
The first airplane working on cryogenic fuel was developed in the USSR in early 1980s on the basis of the passenger aircraft Tu-154. It was then modified using a hydrogen engine installed instead of one of the three kerosene engines.
A. I. Ivanov   +2 more
doaj   +1 more source

Simulation and Application of a New Multiphase Flow Ablation Test System for Thermal Protection Materials Based on Liquid Rocket Engine

open access: yesAerospace, 2022
Internal flow field ablation is an important issue in thermal protection materials for rocket engines and hypersonic vehicles. In this paper, a new multiphase flow ablation test system, with an Al2O3 particle delivery device based on an oxygen-kerosene ...
Qingdong Su   +6 more
doaj   +1 more source

Effects of Compounds in Liquefied Methane on Rocket Engine Operation

open access: yesAerospace, 2022
Methane (CH4) is a promising rocket fuel for various future space mission scenarios. It has advantages in terms of cost, performance, and environmental friendliness.
Jan van Schyndel   +4 more
doaj   +1 more source

On the efficiency of using the Navier-Stokes approximation in thermogasdynamic calculation of low-thrust liquid-propellant rocket engines at low Reynolds numbers

open access: yesВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2022
A numerical method for thermogasdynamic calculation of low-thrust liquid rocket engines is presented. These engines are used as end organs of the system of space attitude control for nanosatellites and small spacecraft.
A. D. Maksimov, S. A. Shustov
doaj   +1 more source

Parametric Simulation Study of Liquid Film Cooling of Hydrocarbon Liquid Rocket Engine

open access: yesAerospace
The hydrocarbon liquid rocket engine working environment is harsh; the thrust chamber needs to withstand high temperatures and a high-pressure working environment, and the thrust chamber wall material is difficult to bear, so it is necessary to design ...
Huixin Yang   +3 more
doaj   +1 more source

Recent Experimental Efforts on High-Pressure Supercritical Injection for Liquid Rockets and Their Implications

open access: yesInternational Journal of Aerospace Engineering, 2012
Pressure and temperature of the liquid rocket thrust chambers into which propellants are injected have been in an ascending trajectory to gain higher specific impulse.
Bruce Chehroudi
doaj   +1 more source

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