Results 41 to 50 of about 133 (76)

Property Learning-Based Fault Detection for Liquid Propellant Rocket Engine Control Systems [PDF]

open access: yes
Accommodating the dynamic and uncertain operational environments that are typical for aerospace applications, our work focuses on robust fault detection and accurate diagnosis in the context of Liquid Propellant Rocket Engines.
Freiberger, Manuel   +3 more
core   +1 more source

Effects of Lip Thickness and Recess Length on Spray Characteristics in Gas Centered Double Swirl Injector for 400N Methane Rocket Engine [PDF]

open access: yes, 2019
학위논문 (석사)-- 서울대학교 대학원 : 공과대학 기계항공공학부, 2019. 2. 윤영빈.The 400N class small rocket engine is widely used for applications such as apogee engine for geosynchronous satellite or attitude control engine for manned or unmanned spacecraft.
이예승
core  

Mathematical model for heat transfer in variable thickness fins for rocket engines [PDF]

open access: yes
Purpose. This article aims to develop a mathematical model for a fin in the cooling system of liquid propellant rocket engines. The objective is to enable calculations for fins with arbitrary thickness variation.
Valerii Bucharskyi, Volodymyr Sliusariev
core   +1 more source

Designing and optimization of pressurizing gas diffusers in cryogenic methane tank: a technical approach [PDF]

open access: yes
openThis paper presents a methodology for the sizing and subsequent optimization of the inert pressurizing gas injection element in a cryogenic tank. The study consists of several steps, starting from the operating conditions, by means of a 0-dimensional
CASARA, RICCARDO
core  

Comparison of GCH4/GOX rocket combustion chambers [PDF]

open access: yes, 2016
LAUREA MAGISTRALEThis thesis aims to compare two different subscale combustion chambers, operating with a pro- pellant combination of gaseous methane (GCH4) and gaseous oxygen (GOx). In the current study, results from an experimental investigation on a
SCAGLIONE, VALERIA
core  

Regression rate determination of a gas generator hybrid rocket motor with GOX [PDF]

open access: yes, 2015
Hybrid rocket motors suffer from low regression rates when compared to traditional solid rocket motors. This work investigates the regression rate of a mixed oxidizer hybrid motor using a fuel-rich solid grain with and without gaseous oxygen as an ...
Mascaro, Michael D.
core   +1 more source

Solution of current problems in the dynamics of hydromechanical and vibration protection systems [PDF]

open access: yes, 2018
Целью данной статьи является обзор основных результатов решения современных задач динамики жидкостных ракетных двигателей (ЖРД), продольной устойчивости жидкостных ракет-носителей (РН), динамики виброзащитных систем, газодинамики лопаточных машин и ...
Довготько, Н.И.   +1 more
core   +1 more source

Design and development of a regenerative cooling for small liquid engines [PDF]

open access: yes
The research work carried out has been focused on the design and development of a regenerative cooling system applied to small liquid rocket engines. According to the "green philosophy" the pair of propellants used are diesel and HTP.

core  

Identifying feedback directions in the mechanisms driving self-sustained thermoacoustic instability in a single-element rocket combustor

open access: yes
The occurrence of high frequency (>1000 Hz) thermoacoustic instability (TAI) sustained by mutual feedback among the acoustic field, heat release rate oscillations, and hydrodynamic oscillations poses severe challenges to the operation and structural ...
Anderson, William   +5 more
core   +1 more source

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