Engineering Journal: Science and InnovationELECTRONIC SCIENCE AND ENGINEERING PUBLICATION
Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Search by keyword: "combustion chamber"


Computation study of the low-thrust rocket engine chamber thermal state operating on the oxygen + methane gaseous propellant components with the structural elements regenerative external cooling by an oxidizer

Published: 01.11.2024

Authors: Novikov A.V., Andreev E.A., Bardakova E.I.

Published in issue: #11(155)/2024

DOI: 10.18698/2308-6033-2024-11-2402

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Computational study of the various mixture formation schemes and determination of the main factors influencing the working process parameters of the low-thrust rocket engine combustion chamber

Published: 07.12.2023

Authors: Novikov A.V., Andreev E.A., Bardakova E.I.

Published in issue: #12(144)/2023

DOI: 10.18698/2308-6033-2023-12-2325

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Design and development of mechanical processing technology to obtain turbulators in the liquid-propellant rocket engine combustion chamber

Published: 20.04.2023

Authors: Yukhnevich S.S., Ryazantsev A.Yu., Evchenko I.V.

Published in issue: #4(136)/2023

DOI: 10.18698/2308-6033-2023-4-2267

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Highly efficient technologies for obtaining small diameter holes in liquid propellant rocket engine parts

Published: 24.03.2023

Authors: Lomakin I.V., Yukhnevich S.S., Ryazantsev A.Yu., Shirokozhukhova A.A.

Published in issue: #3(135)/2023

DOI: 10.18698/2308-6033-2023-3-2258

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Experimental-analytical study of the occurrence of fuel splash through the air intake pipe of the emulsion atomizer

Published: 28.07.2022

Authors: Niazbaev K.T., Ivchenkova I.A., Kudryavtsev V.A., Kudryavtsev A.V.

Published in issue: #7(127)/2022

DOI: 10.18698/2308-6033-2022-7-2194

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts