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A Method for Real-Time Fault Detection of Liquid Rocket Engine Based on Adaptive Genetic Algorithm Optimizing Back Propagation Neural Network. [PDF]

open access: yesSensors (Basel), 2021
A real-time fault diagnosis method utilizing an adaptive genetic algorithm to optimize a back propagation (BP) neural network is intended to achieve real-time fault detection of a liquid rocket engine (LRE).
Yu H, Wang T.
europepmc   +3 more sources

Measurement of Rocket Engine Noise [PDF]

open access: bronzeThe Journal of the Acoustical Society of America, 1960
The measurement of rocket engine noise has become a part of many recent missile and space vehicle development programs. The circumstances under which these measurements must be made, and the type of information desired, present the acoustician with several unique problems in acquiring and interpreting his data. This paper suggests a general approach to
David N. Keast
openaire   +3 more sources

Anomaly Detection Method for Rocket Engines Based on Convex Optimized Information Fusion. [PDF]

open access: yesSensors (Basel)
The power system, as a core component of a launch vehicle, has a crucial impact on the reliability and safety of a rocket launch. Due to the limited measurement information inside the engine, it is often challenging to realize fast and accurate anomaly ...
Sun H, Cheng Y, Jiang B, Lu F, Wang N.
europepmc   +2 more sources

Analysis of properties of inertia regulator of thrust control system of liquid rocket engine [PDF]

open access: yesОмский 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

THERMAL PROTECTION SOLUTION FOR SOLID FUEL ROCKET ENGINES [PDF]

open access: yesAdvanced Engineering Letters, 2023
This paper presents a new approach to the thermal protection of solid-fuel rocket engines. The method of thermal protection using coatings not only reduces the risk of damage to the engine casing but also increases the engine’s efficiency in working ...
Nguyen Minh Phu   +2 more
doaj   +1 more source

Dynamic & Non-linear Modelling of an Expansion Cycle Rocket Engine [PDF]

open access: yesفصلنامه علوم و فناوری فضایی, 2020
Expansion cycle rocket engines have unintelligible and sensitive dynamic behavior. Contrary to other types of rocket engine which have gas generator, Expansion cycle rocket engines utilizes mass flow of fuel propellant to provide power for rotating turbo
Mohammad Amin Eskandari   +3 more
doaj   +1 more source

A Load-Carrying Capacity Evaluation Method for the Welded Joints of Rocket Engine Frame

open access: yesAerospace, 2023
The load-carrying capacities of welded joints need to be paid attention to in the design of the frame, which transfers the thrust generated by the rocket engine to the rocket body.
Yushan Gao   +3 more
doaj   +1 more source

Joint design and simulation of GOX-GCH4 combustion and cooling in an experimental water-cooled subscale rocket engine [PDF]

open access: yesINCAS Bulletin, 2023
This paper presents the authors’ most recent research regarding the feasibility of cooling a 1 kN scaled-down experimental rocket engine, running on gaseous oxygen and gaseous methane, for a ground test.
Alexandru MEREU, Dragos ISVORANU
doaj   +1 more source

Performances Study of a Hybrid Rocket Engine [PDF]

open access: yesINCAS Bulletin, 2018
This paper presents a study which analyses the functioning and performances optimization of a hybrid rocket engine based on gaseous oxygen and polybutadiene polymer (HTPB).
Adrian-Nicolae BUTURACHE
doaj   +1 more source

Thrust performance of the rocket-based combined-cycle engine under ejector mode

open access: yesAIP Advances, 2023
The Rocket-Based Combined-Cycle (RBCC) engine integrates the preponderance of ramjet and rocket engines. It can perform excellently at a lower Mach number than a ramjet while consuming less fuel than the rocket.
Yizhi Yao   +9 more
doaj   +1 more source

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