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: "rocket engine"


Determining structural and technological parameters of the polymer films winding process for pipelines

Published: 17.01.2020

Authors: Nekhoroshikh G.E.

Published in issue: #1(97)/2020

DOI: 10.18698/2308-6033-2020-1-1952

Category: Metallurgy and Science of Materials | Chapter: Powder Metallurgy and Composite Materials

Analysis of the existing igniter devices and the development of a promising igniter design for the launching booster of modern solid-propellant ramjets

Published: 23.05.2019

Authors: Sorokin V.A., Mokretsova O.V., Valuy P.V., Fedorov D.Yu., Molodtsov A.N., Vasin V.A.

Published in issue: #5(89)/2019

DOI: 10.18698/2308-6033-2019-5-1879

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

Analysis of the existing igniter devices and the development of a promising igniter design for the launching booster of modern solid-propellant ramjets

Published: 23.05.2019

Authors: Sorokin V.A., Mokretsova O.V., Valuy P.V., Fedorov D.Yu., Molodtsov A.N., Vasin V.A.

Published in issue: #5(89)/2019

DOI: 10.18698/2308-6033-2019-5-1879

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

Mathematical simulation of the cyclic mode of operation for a liquid propellant spacecraft rocket engine

Published: 11.10.2018

Authors: Ulybyshev S.Yu.

Published in issue: #10(82)/2018

DOI: 10.18698/2308-6033-2018-10-1813

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

Mathematical simulation of the cyclic mode of operation for a liquid propellant spacecraft rocket engine

Published: 11.10.2018

Authors: Ulybyshev S.Yu.

Published in issue: #10(82)/2018

DOI: 10.18698/2308-6033-2018-10-1813

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

Parameter calculation and design of an autonomous thermal cutting machine based on the combustion chamber of a low-thrust rocket engine

Published: 17.01.2018

Authors: Andreev E.A., Krylov V.I., Novikov A.V., Shatsky O.E.

Published in issue: #1(73)/2018

DOI: 10.18698/2308-6033-2018-1-1718

Category: Mechanical Engineering and Machine Science | Chapter: Technology and Equipment of Mechanical and Physical Processing