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Simulation and Analysis of Structural Dynamic Characteristics of Large Thermal Shields of the Space Telescope
| Authors: Golubev E.S., Galinovsky A.L., Arkhipov M.U. | Published: 11.02.2016 |
| Published in issue: #2(671)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: space telescope, thermal shields, large space structures, dynamic performance, mathematic simulation |
Numerical Analysis of the Thermal State of the Resonator in a Gas-Dynamic Ignition System with Two-Phase Fuel Composition
| Authors: Vorozheeva O.A., Arefyev K.Yu. | Published: 11.05.2016 |
| Published in issue: #5(674)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: thermal state, gas-dynamic ignition system, two-phase fuel composition, mathematical modeling, ethanol, temperature field, resonator, pulsed mode |
The Analysis of Influence of the Nozzle Structure and Fluid Injection Path on the Efficiency of Two-Phase Mixing in a Constant Cross Section Channel
| Authors: Arefyev K.Yu., Voronetskiy A.V., Prokhorov A.N., Suchkov S.A., Filimonov L.A. | Published: 30.06.2016 |
| Published in issue: #7(676)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: mathematical modeling, fuel injection, droplet fragmentation, droplet evaporation, constant section channel |
Profiling of the Turbo Compressor Inlet Nozzle of an Aircraft Engine
| Authors: Grishin Yu.A., Buzin A.V., Semenchukova V.S. | Published: 10.08.2016 |
| Published in issue: #8(677)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: aircraft diesel engine, radial compressor, inlet nozzle, computational simulation |
The Study of Shrinkage of Drilled Holes in Polymer Composite Materials
| Authors: Dudarev A.S. | Published: 10.08.2016 |
| Published in issue: #8(677)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: drilling, hole, polymer composite, shrinkage, polygon mesh |
Metal Power Compositions for the EP648 Heat Resistant Alloy Manufactured by All-Russian Research Institute for Aircraft Materials VIAM for Selective Laser Melting, Laser Metal Deposition and Metal Injection Molding Technologies
| Authors: Kablov E.N., Evgenov A.G., Ospennikova O.G., Semenov B.I., Semenov A.B., Korolev V.A. | Published: 07.09.2016 |
| Published in issue: #9(678)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: selective laser melting, laser metal deposition, powder injection molding, metal powder composition, protection environment, mechanical characteristics, hardening, phase |
A New Approach to Measure Spacecraft Moments of Inertia Based on the Analysis of a Self-Oscillating System
| Authors: Reznik S.V., Videnkin N.A. | Published: 07.09.2016 |
| Published in issue: #9(678)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: moment of inertia, spacecraft, self-oscillations |
Information Stability of an Automated Flight Control System for Spacecraft as an Integrated Property Defining its Quality
| Authors: Andreev А.G., Kazakov G.V., Koryanov V.V. | Published: 12.10.2016 |
| Published in issue: #10(679)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: automated control system, restorability, information security, quality, space vehicle, operating and technical level, stability |
Key Properties of Information Stability of an Automated Flight Control System for Spacecraft
| Authors: Andreev А.G., Kazakov G.V., Koryanov V.V. | Published: 24.11.2016 |
| Published in issue: #11(680)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: database, information security, information stability, restorability, operating-technical level, data preparation |
The Methods of Designing a Polymer Composite Wing Using Parametrical Modeling. Part 1. The Rationale for Selecting Wing Geometry and the Calculation of Airloads
| Authors: Mikhailovskiy K.V., Baranovski S.V. | Published: 24.11.2016 |
| Published in issue: #11(680)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: airliner, wing, polymer composite materials, structural arrangement, airloads |