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Key issues of creating the inflatable braking devices for removal of the failed satellites into the atmosphere dense layers Part 1. Conceptual design. Motion in the rarefied atmosphere
Authors: Reznik S.V., Abramova E.N. | Published: 28.04.2023 |
Published in issue: #5(758)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: space debris, near-Earth space cleanup, inflatable braking device, polymer films, rarefied atmosphere, motion simulation |
Plane motion dynamics of a space-based crane-manipulator of the arm type taking into account the links’ bending
Authors: Russkikh S.V., Shklyarchuk F.N. | Published: 10.05.2023 |
Published in issue: #5(758)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: crane-manipulator of the arm type, plane motion dynamics, elastic oscillations, equations in generalized coordinates |
Key issues of creating the inflatable braking devices for removal of the failed satellites into the atmosphere dense layers Part 2. Analysis of the thermal regime under the combined heating conditions
Authors: Reznik S.V., Abramova E.N. | Published: 30.05.2023 |
Published in issue: #6(759)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: space debris, nanosatellite removal, inflatable braking device, polymer films, temperature state simulation, thermal mode |
Selection of the optimal thrust-to-weight ratio of the first stages of small-lift launch vehicles
Authors: Mukhamedov L.P., Kirievskii D.A. | Published: 04.06.2023 |
Published in issue: #6(759)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: ballistic design problem, ballistic design parameters, ultralight launch vehicle, small spacecraft, characteristic velocity losses |
Methods and techniques used in increasing gas temperature in front of the gas turbine engine turbine
Authors: Pismennyi V.L. | Published: 05.06.2023 |
Published in issue: #6(759)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: heat resistance of materials, blade cooling, gas temperature, circulating heat exchanger, heat-shielding coatings, gas turbine engine, air-liquid cooling |
Experimental installation for the study of the influence of electrostatic fields on heat exchange and the process of sedimentation in motor aviation oil with its forced convection
Authors: Altunin V.A., Lvov M.V., Shchigolev A.A., Yusupov A.A., Yanovskaya M.L. | Published: 22.06.2023 |
Published in issue: #7(760)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
Keywords: |