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All articles by "Prosuntsov P.V."
Development of a concentrated radiation heating facility for testing the high-temperature composite materials
| Authors: Khudorozhko M.V., Prosuntsov P.V. | Published: 19.08.2025 |
| Published in issue: #8(785)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: high-temperature composite materials, halogen lamp, radiation heating bench, concentrated radiation source, elliptical reflector, radiation heat exchange simulation |
Theoretical and numerical determination of the polymer composite material permeability by the multiscale simulation approach. Part 2. GFRP
| Authors: Prosuntsov P.V., Polskiy P.V. | Published: 09.03.2025 |
| Published in issue: #3(780)/2025 | |
| 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 |
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, re entry 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 |