Group-Theoretical Analysis of the Clustered Launch Vehicle Dynamics
Authors: Pavlov A.M. | Published: 03.09.2019 |
Published in issue: #4(127)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: launch vehicle, beam system, symmetry group, vibration frequency, irreducible representation, orthoprojector |
Investigating Crew Maintenance Modes for a Lunar Orbital Spaceport Station
Authors: Pugachenko S.E., Kozedub  D.A. | Published: 05.09.2019 |
Published in issue: #4(127)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
Keywords: lunar orbital station, interplanetary mission system, lunar infrastructure simulation, crew maintenance mode, crew time, transportation vehicle, space tug |
Conjugate Heat Transfer and Estimation of Thermal State of Elements of the Thermal Protection Shield Package
Authors: Tovstonog V.A. | Published: 05.09.2019 |
Published in issue: #4(127)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: radiation heat transfer, radiation shield, emissivity, thermal protection |
Diffraction-Based Investigation Methods in Analysing Plastic Strain Zone Underneath Fracture Surface
Authors: Naprienko S.A., Medvedev P.N., Raevskikh A.N., Popov M.A. | Published: 05.09.2019 |
Published in issue: #4(127)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: titanium alloy ВТ41, X-ray crystallography, plastic strain zone, texture, EBSD, electron backscatter diffraction |
Method of Calculating Carbon Ablation in the Jet of Liquid Rocket Engine Combustion Products
Authors: Gorskiy V.V., Kovalsky M.G., Resh V.G. | Published: 17.10.2019 |
Published in issue: #5(128)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: ablation, thermal protection, carbon materials, combustion products, oxidation, erosion, heat flow |
Non-Motor Test Bench Evaluation of Efficiency of the Exhaust System of Low-Power Internal Combustion Engine of UAV
Authors: Sukhovaya E.A., Telyashov D.A., Pavlov G.I., Nakoryakov P.V., Nikitin M.A. | Published: 17.10.2019 |
Published in issue: #5(128)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: low-power internal combustion engine, exhaust system of engine, muffler, non-motor test bench, weak shock waves in airflow, hydrodynamic resistance, noise attenuation efficiency |
Using the Maximum Pressure Principle for Verification of Calculation of Stationary Subsonic Flow
Authors: Anikin V.A., Vyshinsky V.V., Pashkov O.A., Streltsov E.V. | Published: 20.12.2019 |
Published in issue: #6(129)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: nonlinear partial differential equations, boundary value problems, Euler equations, Reynolds averaged Navier --- Stokes equations, subsonic vortex flows, subsonic maximum pressure principle |
Structure and Heat Resistance of Intermetallic Rhenium-Containing Alloy after Heat Treatment
Authors: Arginbaeva E.G., Bazyleva O.A., Karachevtsev F.N., Nazarkin R.М | Published: 20.12.2019 |
Published in issue: #6(129)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
Keywords: intermetallics, nickel, heat treatment, structure, phase, misfit |
Investigation of the Influence of Structural and Adjusting Parameters of a Quadruple-Orifices Electrohydraulic Amplifier on the Static Characteristics of Rocket Pack Steering Actuator
Authors: Belonogov O.B. | Published: 20.12.2019 |
Published in issue: #6(129)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: structural and adjusting parameters, electrohydraulic amplifier, steering actuator, static characteristics |
Study of Hydraulic Characteristics of the Cooling Path of a Model Liquid Rocket Engine Manufactured using Additive Technology of Selective Laser Melting
Authors: Yagodnikov D.A., Aleksandrenkov V.P., Kovalev K.E., Grigoryants A.G., Drenin    A.A. | Published: 20.12.2019 |
Published in issue: #6(129)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: hydraulic characteristics, cooling path, combustion chamber fins, additive technologies, thermal protection |