Results 81 to 90 of about 25,209 (263)

Erratum to: “Numerical and experimental investigations of the effect of repeated cyclic thermal loads on the strength of materials of recoverable liquid-propellant rocket engines” [PDF]

, 2009
V. I. Bubnov, D. V. Isakov, I. G. Lozino-Lozinskaya, A. M. Polyanskiǐ   +3 more
openalex   +1 more source

Simulation Study on Outflow Characteristics of Cryogenic Propellant during Rocket Ascent

Zhileng xuebao, 2020
At the rocket launching stage, it is very important to supply sufficient and vapor-free liquid propellant to maintain the functioning of the main engine.
Huang Xiaoning, Wang Lei, Mao Hongwei, Xue Liangjiang, Li Yanzhong   +4 more
doaj  

EMF Frequency Response Investigation of Liquid-Propellant Rocket Supersonic Jet [PDF]

, 2012
Д.А. Ягодников, А.В. Рудинский   +1 more
openalex   +1 more source

The problem of combustion instability in liquid rocket engines

Challenges and Issues of Modern Science
The purpose of this work is to carry out an overview on combustion instability in liquid propellant rocket engines, its classification, the main principles of occurrence as well as ways to prevent the phenomena while designing of the prospective engine.
Samir Vekilov, Volodymyr Lipovskyi, Roman Pustovyi   +2 more
doaj  

Application of the substructure method for thermal stress-strain assessment of a liquid-propellant rocket engine combustion chamber [PDF]

, 2013
С.С. Гаврюшин, Е.Е. Красновский, О.В. Короткая, Павел Петрович Стриженко, Р.Э. Катков   +4 more
openalex   +1 more source

IT modeling technologies of credible rocket propellants in liquid rocket engines processes [PDF]

, 2013
Р.Р. Назырова, Н.Б. Пономарев   +1 more
openalex   +1 more source

Development of test stand for experimental investigation of chemical and physical phenomena in Liquid Rocket Engine [PDF]

Journal of Aerospace Technology and Management, 2011
The main objective of this work was to present the specification of an experimental firing test stand for liquid rocket engines (LRE) and develop a program for control and acquisition of data.
Emerson Andrade Santos, Wilton Fernandes Alves, André Neves Almeida Prado, Cristiane Aparecida Martins   +3 more
doaj  

Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines

Acta Astronautica, 2020
W. Armbruster, J. Hardi, Yannik Miene, D. Suslov, M. Oschwald   +4 more
semanticscholar   +1 more source

ON THE STABILITY OF THE STABILIZED MOTION OF A CARRIER ROCKET WITH A LIQUID-PROPELLANT JET ENGINE AND AN ONBOARD DIGITAL COMPUTER IN THE STABILIZATION LOOP

, 2022
Eugene Aleksandrov, Тетяна Александрова, Iryna Kostianyk, Yaroslav Morgun   +3 more
openalex   +2 more sources

Proposals for Improving the Efficiency and Durability of the Turbines of Turbo-Pump Assemblies in Liquid-Propellant Rocket Engines by Using Double-Sided Crest-Type Radial Labyrinth Seals [PDF]

, 2019
V S Vasiliev, Petr Levochkin, Vladimir Chvanov, Sergey Timushev   +3 more
openalex   +1 more source