Development of an Experimental Setup to Study the Load-Carrying Capacity of a Single-Stage Magnetic Rotor Suspension
| Authors: Badykov R.R., Lomachev A.O., Benedyuk M.A., Grigoriev E.M. | Published: 10.12.2022 |
| Published in issue: #4(143)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
| Keywords: magnetic rotor suspension, axial magnet, PID-controller, hybrid magnetic bearing, electronic control system | |
Recuperation of Aircraft Gas Turbine Engines to Solve Problems Land Transport and Energy
| Authors: Benmunach A., Zanabili G., Govorkov A.S. | Published: 11.12.2022 |
| Published in issue: #4(143)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: gas turbine engines, recuperation, compressor, combustion chamber, turbine, output device | |
Convective Heat Transfer and Friction in a Thin Laminar-Turbulent Boundary Layer on the Permeable Surface of a Blunted Cone of Small Elongation
| Authors: Gorskiy V.V., Savvina A.G. | Published: 12.12.2022 |
| Published in issue: #4(143)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: сonvective heat transfer, friction, momentum loss thickness, boundary layer | |
Estimates of Equilibrium Temperature on the Surface of the Spherical Blunt of the Descent Orbiter
| Authors: Zarubin V.S., Zimin V.N. , Leonov V.V., Zarubin V.S. jr. | Published: 12.12.2022 |
| Published in issue: #4(143)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: equilibrium temperature, free molecular flow mode, continuum flow mode, Knudsen number | |
High-Precision Aircraft Guidance System with Axial Acceleration Self-Tuning
| Authors: Klishin A.N., Kolesnikova D.S. | Published: 14.12.2022 |
| Published in issue: #4(143)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: adaptive guidance system, homing, stabilization system, aircraft, mathematical simulation | |
Approach to Reducing Vibroactivity of Small Spacecraft
| Authors: Biryukova M.V., Tufan A., Ermakov V.Yu. | Published: 26.03.2023 |
| Published in issue: #1(144)/2023 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: electric motor-flywheel, non-contact electric motor-flywheel, vibration isolator, imbalance, disturbing factors, vibration activity | |
The Algorithm of Gas Dynamic Calculation on Asymmetric Cones by the Method of Local Wedges and Cones
| Authors: Gorskiy V.V., Brodskiy M.Yu. | Published: 27.03.2023 |
| Published in issue: #1(144)/2023 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: problems of spatial flow, laminar turbulent heat transfer, boundary layer, method of local wedges and cones | |
Estimation of the Rejection Boundaries of the Spacecraft Schematic Layout by Thermal and Erosive Effects Level of the Electric Rocket Engines Plasma Jets
| Authors: Nadiradze А.B., Dudunov А.А. | Published: 27.03.2023 |
| Published in issue: #1(144)/2023 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: electric rocket engine, plasma jet, thermal effect, erosive effect, allowable effect level, rejection boundary | |
Experimental Study of the Carbon Deposits Accumulation in the Oxygen-Methane Model Gas Path
| Authors: Fedorov S.A., Slesarev D.F., Isakov D.V. | Published: 27.03.2023 |
| Published in issue: #1(144)/2023 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: liquid propellant rocket engine, reducing generator gas, carbon deposits, soot | |
The Concept of Constructing a Stand to Test the SpaceWire Onboard Equipment with Possibility of Software and Hardware Simulation of Reconfigurable Topology of the Spacecraft Onboard Network
| Authors: Maksyutin A.S., Murygin A.V. | Published: 23.06.2023 |
| Published in issue: #2(145)/2023 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: test stands, test methods, spacecraft, onboard networks, SpaceWire | |