Results 11 to 20 of about 20,668 (233)
Energies, 2022 The successful design of a liquid rocket engine is strictly linked to the development of efficient cooling systems, able to dissipate huge thermal loads coming from the combustion in the thrust chamber.
Daniele Ricci +2 more
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Remaining Useful Life Prediction for Liquid Propulsion Rocket Engine Combustion Chamber
2021 5th International Conference on Control and Fault-Tolerant Systems (SysTol), 2021 The reusability of a liquid propulsion rocket engine (LPRE) has gained tremendous attention in the recent years. The present paper deals with an automatic estimation of the Remaining Useful Life of a LPRE combustion chamber with the cracking of the internal wall due to the thermo-mechanical stress considered as one of the major degradation modes.
Chelouati, Mohammed +3 more
openaire +2 more sources
Life Analysis of Reusable Liquid Rocket Engine Thrust Chamber
Aerospace, 2022 The thrust chamber’s inner wall suffers high temperature and pressure differences from the coolant channel, which limits the life of the rocket engine.
Yuanjie Qi, Yuqiang Cheng, Yan Zhang
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Effects of swirl number and bluff body on swirling flow dynamics
AIP Advances, 2023 Bluff-body swirling flows have been widely employed in gas-turbine combustors to achieve flame stabilization. Meanwhile, considerable efforts have been made to understand swirling flow dynamics, the effects of swirl number and bluff body on flow ...
Yupeng Gao +4 more
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Modelling Rocket System Performance Parameters
Academy 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
FirePhysChem, 2021 This paper presents the status of developments worldwide regarding use of hybrid rocket motors for space transportation. Historical roots are presented and reasons for revisiting hybrid technology after a few decades of limited interest are examined ...
Adam Okninski +3 more
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A Liquid Launch Vehicle Safety Assessment Model Based on Semi-Quantitative Interval Belief Rule Base
Mathematics, 2022 As the propulsion part of a space launch vehicle and nuclear weapon missile, the health status of the liquid rocket determines whether the space launch vehicle and nuclear weapon missile can function normally.
Xiaoyu Cheng +3 more
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Generative adversarial networks with physical evaluators for spray simulation of pintle injector
AIP Advances, 2021 Due to the adjustable geometry, pintle injectors are especially suitable for liquid rocket engines, which require a widely throttleable range. However, applying the conventional computational fluid dynamics approaches to simulate the complex spray ...
Hao Ma +3 more
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Liquid Propulsion at IAE: Vision of the activities and future perspectives [PDF]
Journal of Aerospace Technology and Management, 2009 This paper presents the activities in the area of liquid propulsion, which received an effective boost at the end of the 90s. There is a consensus among specialists on the use of liquid propulsion in the next generation of satellite launcher vehicles in ...
Marco F. Carvalho Torres +4 more
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Supercritical Injection Modeling by an Incompressible but Variable Density Approach
Aerospace, 2023 Supercritical nitrogen jet behavior is modeled using an incompressible but variable density approach developed for variable density jets. Following mechanical and thermal breakup concepts, several injection conditions relevant to liquid rocket propulsion
Leandro B. Magalhães +2 more
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