Search
The Efficiency of Tribocoupling with МоS2-Based Solid Lubricant Coatings Using Magnetron and Suspension Sputtering
Authors: Khopin P.N. | Published: 23.09.2019 |
Published in issue: #9(714)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: solid lubricant coatings, tribotechnical indicators, magnetron and suspension sputtering, high vacuum |
Safe Conditions for Conducting Tests Using Ballistic Facilities
Authors: Gerasimov S.I., Odzeriho I.A., Gerasimova R.V., Salnikov A.V., Kalmykov A.P., Yanenko B.A. | Published: 23.09.2019 |
Published in issue: #9(714)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Inspection and Testing of Aircraft and Aircraft Systems | |
Keywords: aeroballistic testing, gun type launchers, near muzzle and exterior ballistics |
Design and Technology of Winding Curvilinear Pipelines from Sintered Polyimide-Fluoroplastic Film
Authors: Komkov M.A., Badanina Y.V. | Published: 28.10.2019 |
Published in issue: #10(715)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: cryogenic fuel, polyimide film, film shell, curvilinear pipelines, winding method |
Methodology for Determining the Survivability and Resistance of Aircraft Propellers to the Impact of Foreign Objects
Authors: Neskoromnyy Е.V., Markov D.S. | Published: 28.10.2019 |
Published in issue: #10(715)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Inspection and Testing of Aircraft and Aircraft Systems | |
Keywords: blade made of composite materials, damage by foreign objects, propeller, surviv-ability and impact resistance, impact resistance |
Validation of Methods for Calculating Hydrogen Combustion in a Supersonic Model Air Flow Using the Experimental Data of Beach — Evans — Schexnayder
Authors: Kukshinov N.V., Batura S.N., Frantsuzov M.S. | Published: 26.11.2019 |
Published in issue: #11(716)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
Keywords: hydrogen combustion, chemical kinetics, turbulent flow, turbulence models, numerical simulation, supersonic flow |
New Science-Intensive Technologies for Electrophysical and Chemical Treatment of Aerospace Parts
Authors: Kushnarenko S.B., Fomichev A.O., Astakhov Y.P., Bogdanov K.A., Perepechkin A.A., Belov I.I. | Published: 26.11.2019 |
Published in issue: #11(716)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: hybrid technologies, combined methods, acoustocapillary effect, tool electrode, working fluid, electrical discharge machining |
Methods of Calculation of Performance Indicators of Spacecraft Flight Control Systems
Authors: Panteleymonov I.N., Potyupkin A.Y., Trankov V.M., Panteleymonova A.V., Filatov V.V., Todurkin V.V. | Published: 26.11.2019 |
Published in issue: #11(716)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: communication and control session, spacecraft, mission control center, flight control system, command-measuring station, on-board equipment |
Motion Control of Electric Propulsion Spacecraft Transfers between the Libration Points L1 and L2 of the Earth–Moon System
Authors: Fain M.K., Starinova O.L. | Published: 26.11.2019 |
Published in issue: #11(716)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: spacecraft, low thrust engine, sequential linearization method, Earth–Moon system, libration point |
Methods of Creating Functional Models of Gas Turbine Engine Parts by Means of Numerical Modeling and Machine Learning Algorithms Using a Turbine Disk as an Example
Authors: Reznik S.V., Sapronov D.V., Vasilyev B.E., Semenov A.V. | Published: 26.11.2019 |
Published in issue: #11(716)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: gas turbine engine, turbine disk, functional model, machine learning |
Methodological Aspects of Determining Thrust of Irrotational Air-Breathing Jet Engines in Bench and Flight Tests
Authors: Semenov V.L., Aleksandrov V.Yu., Prokhorov A.N., Arefyev K.Yu., Kruchkov S.V. | Published: 26.11.2019 |
Published in issue: #11(716)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Inspection and Testing of Aircraft and Aircraft Systems | |
Keywords: irrotational air-breathing jet engine, high-speed aircraft, engine thrust, specific impulse, pressure loading, numerical model |