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Material science problems of building space antennas with a transformable reflector 100 m in diameter

IOP conference series. Materials Science and Engineering, 2016-10, Vol.153 (1), p.12001

2016

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Parametric and topology optimization of polymer composite load bearing elements of rear part of aircraft fuselage structure

AIP Conference Proceedings, 2021, Vol.2318 (1)

2021

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Re-entry trajectory design for reusable spaceplane of tourist class

AIP Conference Proceedings, 2021, Vol.2318 (1)

2021

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Determining loads on small space debris trap’s load-bearing frame in case of hypervelocity impact

AIP Conference Proceedings, 2021, Vol.2318 (1)

2021

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History and experience of overcoming thermal barriers in rocket and space technology: 1. Ballistic missiles

IOP conference series. Materials Science and Engineering, 2020-11, Vol.971 (5), p.52047

2020

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Parametric and topology optimization of load bearing elements of aircraft fuselage structure

IOP conference series. Materials Science and Engineering, 2020-09, Vol.934 (1), p.12029

2020

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Thermal regime of large space structure with transformable elements from hybrid composite

Journal of physics. Conference series, 2018-11, Vol.1134 (1), p.12048

2018

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Study variants of hard CFRP reflector for intersatellite communication

IOP conference series. Materials Science and Engineering, 2016-10, Vol.153 (1), p.12012

2016

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Coupled CFD-based Shape Optimization of a Wing of Reusable Space Vehicle of Tourist Class

IOP conference series. Materials Science and Engineering, 2020-01, Vol.709 (2), p.22108

2020

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Evaluation the complex of thermal properties for epoxy-based GFRP used in wing of tourist class reusable space vehicle

IOP conference series. Materials Science and Engineering, 2020-09, Vol.934 (1), p.12059

2020

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Multiscale modeling of the binder polymer composite materials heating using microwave radiation

Journal of physics. Conference series, 2018-11, Vol.1134 (1), p.12047

2018

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Hybrid composites in reusable space vehicles wing structures

IOP conference series. Materials Science and Engineering, 2019-11, Vol.683 (1), p.12067

2019

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Thermophysical processes models in composite workpieces processed by microwave radiation

IOP conference series. Materials Science and Engineering, 2019-11, Vol.683 (1), p.12029

2019

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Analysis of thermal stabilization process for organomorphic preforms made of oxidized polyacrylonitrile

IOP conference series. Materials Science and Engineering, 2020-01, Vol.709 (2), p.22114

2020

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Heat and Mass Transfer in the Chemical Vapor Deposition of Silicon Carbide in a Porous Carbon–Carbon Composite Material for a Heat Shield

Journal of engineering physics and thermophysics, 2017-03, Vol.90 (2), p.291-300

2017

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Matrix curing in the workpieces made of polymer composites using microwave radiation

IOP conference series. Materials Science and Engineering, 2020-09, Vol.934 (1), p.12027

2020

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Development of the radiant heating facilities for the testing of ceramic materials with operating temperatures up to 2000 K

IOP conference series. Materials Science and Engineering, 2019-11, Vol.683 (1), p.12062

2019

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Numerical Simulation of a Thermal-Protection Element of a Promising Reusable Capsule-Type Lander

Journal of engineering physics and thermophysics, 2017, Vol.90 (1), p.110-116

2017

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Determination of the effect of carbon nanosized particles on thermophysical characteristics of polymer composite materials

Polymer science. Series D, Glues and sealing materials, 2016-10, Vol.9 (4), p.377-381

2016

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Optimal Thermal Design of a Multishield Thermal Protection System of Reusable Space Vehicles

Journal of engineering physics and thermophysics, 2016-03, Vol.89 (2), p.528-533

2016

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Comparison of space antennas mirror reflectors parameters made of composite materials

MATEC Web of Conferences, 2017, Vol.110, p.1072

2017

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Investigation of a ceramic vane with a metal disk thermal and mechanical contact in a gas turbine impeller

EPJ Web of Conferences, 2015, Vol.82, p.1034-1-01034-6

2015

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Analysis of combined radiation-conductive heat transfer during destruction of porous carbon-ceramic matrix composite material of thermal protection

AIP Conference Proceedings, 2021, Vol.2318 (1)

2021

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Wing box topology optimization of tourist class reusable space vehicle

AIP conference proceedings, 2019, Vol.2171 (1)

2019

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Wing airfoil selection and optimization for the tourist class reusable space vehicle

AIP Conference Proceedings, 2019, Vol.2135 (1)

2019

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Material science problems of building space antennas with a transformable reflector 100 m in diameter

Parametric and topology optimization of polymer composite load bearing elements of rear part of aircraft fuselage structure

Re-entry trajectory design for reusable spaceplane of tourist class

Determining loads on small space debris trap’s load-bearing frame in case of hypervelocity impact

History and experience of overcoming thermal barriers in rocket and space technology: 1. Ballistic missiles

Parametric and topology optimization of load bearing elements of aircraft fuselage structure

Thermal regime of large space structure with transformable elements from hybrid composite

Study variants of hard CFRP reflector for intersatellite communication

Coupled CFD-based Shape Optimization of a Wing of Reusable Space Vehicle of Tourist Class

Evaluation the complex of thermal properties for epoxy-based GFRP used in wing of tourist class reusable space vehicle

Multiscale modeling of the binder polymer composite materials heating using microwave radiation

Hybrid composites in reusable space vehicles wing structures

Thermophysical processes models in composite workpieces processed by microwave radiation

Analysis of thermal stabilization process for organomorphic preforms made of oxidized polyacrylonitrile

Heat and Mass Transfer in the Chemical Vapor Deposition of Silicon Carbide in a Porous Carbon–Carbon Composite Material for a Heat Shield

Matrix curing in the workpieces made of polymer composites using microwave radiation

Development of the radiant heating facilities for the testing of ceramic materials with operating temperatures up to 2000 K

Numerical Simulation of a Thermal-Protection Element of a Promising Reusable Capsule-Type Lander

Determination of the effect of carbon nanosized particles on thermophysical characteristics of polymer composite materials

Optimal Thermal Design of a Multishield Thermal Protection System of Reusable Space Vehicles

Comparison of space antennas mirror reflectors parameters made of composite materials

Investigation of a ceramic vane with a metal disk thermal and mechanical contact in a gas turbine impeller

Analysis of combined radiation-conductive heat transfer during destruction of porous carbon-ceramic matrix composite material of thermal protection

Wing box topology optimization of tourist class reusable space vehicle

Wing airfoil selection and optimization for the tourist class reusable space vehicle

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