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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Computational and experimental study of reliability of rocket-engine firing and starting operation of low thruster on the gaseous components oxygen + methane with electric spark ignition

Published: 27.03.2017

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

Published in issue: #4(64)/2017

DOI: 10.18698/2308-6033-2017-4-1606

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

Conditions for gas cavity collapse in fluid during the transition from weightlessness to short-term exposure to individual G-force pulses

Published: 26.12.2016

Authors: Sapozhnikov V.B., Avraamov N.I.

Published in issue: #2(62)/2017

DOI: 10.18698/2308-6033-2017-2-1581

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

Correlation and spectral analyses of electrophysical characteristics of hydrocarbon fuel exhaust products in a model liquid rocket engine

Published: 07.12.2016

Authors: Yagodnikov D.A., Sukhov A.V., Iryanov N.Ya., Lapitsky V.I., Grishin S.A., Bunchuk A.A.

Published in issue: #1(61)/2017

DOI: 10.18698/2308-6033-2017-1-1574

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

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