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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Methodological support and calculation of operational parameters of experimental testing of model rocket-ramjet engines

Published: 22.11.2016

Authors: Yagodnikov D.A., Sukhov A.V., Iryanov N.Ya.

Published in issue: #12(60)/2016

DOI: 10.18698/2308-6033-2016-12-1562

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

Experimental study of thermal-hydraulic characteristics of combustion chamber cooling channels with critical propulsion plant ribbing parameters

Published: 23.09.2016

Authors: Aleksandrenkov V.P., Zubkov N.N., Yagodnikov D.A., Iryanov N.Ya., Sukhov A.V.

Published in issue: #10(58)/2016

DOI: 10.18698/2308-6033-2016-10-1545

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

Experimental and theoretical study of combustor discharge from the double-nozzled gas generator

Published: 23.09.2016

Authors: Yagodnikov D.A., Arefiev K.Yu., Sukhov A.V., Khomyakov I.I., Iryanov N.Ya.

Published in issue: #10(58)/2016

DOI: 10.18698/2308-6033-2016-10-1544

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

Regulation of the burning rate of a pyrotechnic composition based on magnesium and sodium nitrate additives of different type and particle size

Published: 23.09.2016

Authors: Shibanov S.V., Yagodnikov D.A., Sarabjev V.I., Danilova G.A., Kachaun V.S.

Published in issue: #10(58)/2016

DOI: 10.18698/2308-6033-2016-10-1542

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

Space power propulsion systems with gas turbine power conversion system of closed Brayton cycle of high power and characteristic features of their experimental testing

Published: 15.07.2016

Authors: Andrianov D.I., Zakharenkov L.E., Karevskiy A.V., Popov A.V., Popov S.A., Semenkin A.V., Solodukhin A.E., Terekhov D.N., Shtonda S.Yu.

Published in issue: #7(55)/2016

DOI: 10.18698/2308-6033-2016-7-1518

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