MainCatalogAviation and Rocket-Space EngineeringThermal, Electric Jet Engines, and Power Plants of Aircrafts
Mass-capacity analysis and comparison of power installations under operation conditions on the lunar station
| Authors: Lezhnev A.O. , Mamiy T.V. | Published: 27.04.2023 |
| Published in issue: #3(80)/2023 | |
| DOI: DOI: 10.18698/2541-8009-2023-3-872 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: power plant, lunar station, dual-mode nuclear power plant, thermionic emission reactor-converter, thermos-electrochemical converter, electrochemical generator, photovoltaic converters, mass-power characteristic | |
Solid propellants, their advantages and disadvantages
| Authors: Ibatullin A.R., Melikova T.G. | Published: 21.02.2022 |
| Published in issue: #2(67)/2022 | |
| DOI: DOI: 10.18698/2541-8009-2022-2-768 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: rocket science, cosmonautics, rocket and space technology, history of rocket science, rocket engines, engine design, solid rocket fuel, solid fuel engine, composition of rocket fuels | |
Simulation of hydrogen combustion in a supersonic air flow with the assumption of a single-stage chemical reaction
| Authors: Miroshnichenko S.A. | Published: 17.02.2022 |
| Published in issue: #1(66)/2022 | |
| DOI: DOI: 10.18698/2541-8009-2022-1-762 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: mathematical model, combustion, hydrogen, supersonic combustion chamber, aircraft, assumption, one-stage chemical reaction, distribution | |
A parametric study of the thermal state of a cone with a supersonic airflow
| Authors: Miroshnichenko S.A. | Published: 26.05.2020 |
| Published in issue: #5(46)/2020 | |
| DOI: DOI: 10.18698/2541-8009-2020-5-608 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: cone, airflow, supersonic airflow, mathematical model, convective heat transfer, temperature, thermal state, angle of attack | |
Numerical modeling of the flame tube operation in the cooling system of the air-jet engine combustion chamber
| Authors: Batenin I.A. | Published: 04.09.2019 |
| Published in issue: #8(37)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-8-516 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: ramjet engine, combustion chamber, flame tube, film cooling, mathematical modeling, fluid and gas dynamics, cooling jacket, air intake | |
Features of obtaining liquid oxygen for liquid fuel rocket engines
| Authors: Kalugin K.S. | Published: 06.06.2019 |
| Published in issue: #6(35)/2019 | |
| DOI: DOI: 10.18698/2541-8009-2019-6-488 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: liquid fuel rocket engine, oxygen, oxidizer, rocket engine, liquid rocket fuel, cooling, coolant, cryogenic component, chemical fuel | |
Review of experimental studies of the efficiency of film cooling of a flat surface
| Authors: Melnikov A.I. | Published: 20.11.2018 |
| Published in issue: #11(28)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-11-407 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: film cooling, efficiency of film cooling, flat surface, measured data, blowing of cooler, line of bore, adiabatic wall, verification | |
Application of multipropellant fuel in rocket engines
| Authors: Kalugin K.S. | Published: 27.04.2018 |
| Published in issue: #5(22)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-5-304 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: rocket fuel, multipropellant fuel, pseudoliquified powdered metalized fuel, aerojet engine, hydro jet engine, chemical fuel, liquid rocket engine | |
Usage of oxygen-and-methane propellant in liquid-propellant rocket engines
| Authors: Bregvadze D.T., Gabidulin O.V., Gurkin A.A., Zabolotko I.A. | Published: 29.11.2017 |
| Published in issue: #12(17)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-12-205 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: liquid-propellant rocket engines, liquid methane, prospective rocket fuel, cooling of rocket engine, fuel-to-oxidizer ratio | |