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All articles by "Prosuntsov P.V."
Theoretical and numerical determination of the polymer composite material permeability by the multiscale simulation approach. Part 1. GFRP
Authors: Prosuntsov P.V., Polskiy P.V. | Published: 13.08.2024 |
Published in issue: #8(773)/2024 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: polymer composite material, fiberglass homogeneous characteristics, dielectric characteristics, representative volume element, multiscale simulation, electromagnetic radiation |
Analyzing thermal state of the Buran orbital space vehicle structure in the areas of possible damages to its thermal protection elements
Authors: Timoshenko V.P., Prosuntsov P.V., Reznik S.V. | Published: 10.06.2024 |
Published in issue: #6(771)/2024 | |
Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
Keywords: thermal protection, fibrous ceramics, felt substrate, thermal conductivity coefficient, thermal destruction, metal skin melting |
Method of designing the composite load-bearing elements of the fuselage tail section
Authors: Tun Lin Htet, Prosuntsov P.V. | Published: 09.02.2023 |
Published in issue: #2(755)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: light aircraft, fuselage tail section, power structure, parametric optimization, topological optimization, polymer composite material |
Employment of an Active Thermal Control System for Developing a Space-Based Antenna Complex Reflector
Authors: Azhevsky Ya.A., Prosuntsov P.V. | Published: 20.03.2022 |
Published in issue: #4(745)/2022 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: radar survey, Earth remote sensing, active thermal control system, sandwich panels, orbital flight, carbon heaters |
Simulation of Small-Size Space Debris Impact on the Protective Shield of a Transformable Trap
Authors: Prosuntsov P.V., Alekseev A.A., Zherebtsova E.O. | Published: 28.10.2021 |
Published in issue: #11(740)/2021 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: spacecraft, space debris, spacecraft shielding, composite materials, hypervelocity impact, Smooth Particle Hydrodynamics |
Design Optimization of Shape and Layup Sequence of Polymer Composite Load Bearing Elements of Light Aircraft
Authors: Tun Lin Htet, Prosuntsov P.V. | Published: 20.08.2021 |
Published in issue: #9(738)/2021 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: tail section, fuselage, load bearing ribs, parametric optimization, topological optimization method, mass reducing, structural layout |
Wing Shape Optimization and Selecting Rational Re-Entry Trajectory for Reusable Spacecraft of Tourist Class
Authors: Ashikhmina E.R., Prosuntsov P.V. | Published: 23.07.2021 |
Published in issue: #8(737)/2021 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: reusable spacecraft, space tourism, trajectory control, reentry trajectory design, shape optimization |
An Analysis of Combined Radiation-Conductive Heat Transfer During the Destruction of Porous Carbon-Ceramic Composite Material of the Thermal Protection Shield
Authors: Prosuntsov P.V., Barinov D.Y. | Published: 13.12.2020 |
Published in issue: #12(729)/2020 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: mathematical model, descent module, thermal protection, radiation- conductive heat transfer |
Modeling the Heating of the Binder of Polymeric Composite Materials Using Microwave Radiation
Authors: Prosuntsov P.V., Reznik S.V., Mikhailovskiy K.V., Belenkov E.S. | Published: 24.12.2018 |
Published in issue: #12(705)/2018 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: rocket and space technology, polymer composite material, binder curing, microwave radiation, representative volume element |
Prospects of Increasing the Dimensional Stability and the Weight Efficiency of Mirror Space Antenna Reflectors Made of Composite Materials
Authors: Reznik S.V., Prosuntsov P.V., Novikov A.D. | Published: 24.01.2018 |
Published in issue: #1(694)/2018 | |
Category: Aviation, Rocket and Technology | |
Keywords: mirror space antenna reflector, composite materials, carbon fiber reinforced plastic, thermomechanical analysis |