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: "liquid-propellant rocket engine"


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

Prospects of introducing combined porous mesh materials in the in-tank device structures of the spacecraft and upper stage propulsion systems

Published: 24.03.2023

Authors: Korolkov A.V., Polyanskiy A.R., Sapozhnikov V.B.

Published in issue: #3(135)/2023

DOI: 10.18698/2308-6033-2023-3-2260

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

On the S-25 anti-aircraft missile system. Part 2

Published: 19.01.2022

Authors: Metelsky A.O., Markov V.A., Pusev V.I.

Published in issue: #1(121)/2022

DOI: 10.18698/2308-6033-2022-1-2144

Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft

Experimental study of thermal processes in gaseous methane at its natural convection

Published: 18.05.2021

Authors: Altunin V.A., Altunin K.V., Abdullin M.R., Chigarev M.R., Aliev I.N., Yanovskaya M.L.

Published in issue: #5(113)/2021

DOI: 10.18698/2308-6033-2021-5-2080

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

Calculation of minimum supply of fuel in contact with the innertank device to ensure the operation of a liquid-propellant rocket engine in zero gravity

Published: 24.03.2021

Authors: Sapozhnikov V.B., Polyanskiy A.R., Korolkov A.V.

Published in issue: #3(111)/2021

DOI: 10.18698/2308-6033-2021-3-2063

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

Innovative methodology for calculation and design of liquid-propellant rocket engine combustion chamber

Published: 21.11.2016

Authors: Korotkaya O.V.

Published in issue: #12(60)/2016

DOI: 10.18698/2308-6033-2016-12-1560

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

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

Published: 08.10.2013

Authors: Gavrushin S.S., Krasnovskiy E.E., Korotkaya O.V., Strizhenko P.P., Katkov R.E.

Published in issue: #4(16)/2013

DOI: 10.18698/2308-6033-2013-4-705

Category: Engineering | Chapter: Rocket and space technology