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Aerospace vehiclesSemantic difficulties of the English aerospace terminological system

Semantic difficulties of the English aerospace terminological system

Semantic difficulties of the English aerospace terminological system Irina Suima ORCID: https://orcid.org/0000-0002-2209-8614 Oles Honchar Dnipro National University The Purpose of the research is to describe the modern system of astronomical and rocket engineering terminology and to investigate the peculiarities of the translation of the relevant terms into the Ukrainian language. Research Methods: methods of linguistic analysis, descriptive and comparative methods, methods of classification and systematization. Findings: The aerospace terminological system does not exist separately from the terminological systems of other …

Aerospace vehiclesSynthesis of design and technological solutions in the development of UAV launch system

Synthesis of design and technological solutions in the development of UAV launch system

Synthesis of design and technological solutions in the development of UAV launch system Artem Shvets ORCID: https://orcid.org/0009-0006-7637-9143 Oles Honchar Dnipro National University Ihor Bilotserkovskyi ORCID: https://orcid.org/0009-0009-5102-7864 Oles Honchar Dnipro National University Oleksii Kulyk ORCID: https://orcid.org/0000-0002-2913-4462 Oles Honchar Dnipro National University Oleksandr Dobrodomov ORCID: https://orcid.org/0009-0005-9926-6638 Oles Honchar Dnipro National University This scientific paper examines the process of launching unmanned aerial vehicles (UAVs) using a solid-fuel rocket engine. The primary focus is on analyzing the design and technological aspects and advantages of …

Aerospace vehiclesEvaluation of the feasibility of using aerodynamic de-orbiting systems depending on the orbit altitude

Evaluation of the feasibility of using aerodynamic de-orbiting systems depending on the orbit altitude

Evaluation of the feasibility of using aerodynamic de-orbiting systems depending on the orbit altitude Anatolii Abaturov ORCID: https://orcid.org/0009-0007-7402-3909 Oles Honchar Dnipro National University This article is devoted to analyzing and evaluating the feasibility of using aerodynamic systems for space object deorbiting depending on the orbital altitude. The study’s main purpose is to determine the orbital altitude at which the use of aerodynamic systems is appropriate. In the process of research were analyzed modern scientific works devoted to developing such systems. …

Aerospace vehiclesUAV launch methods

UAV launch methods

UAV launch methods Oleksandr Dobrodomov ORCID: https://orcid.org/0009-0005-9926-6638 Oles Honchar Dnipro National University Vladyslav Proroka ORCID: https://orcid.org/0000-0001-6884-3934 Oles Honchar Dnipro National University Oleksii Kulyk ORCID: https://orcid.org/0000-0002-2913-4462 Oles Honchar Dnipro National University Unmanned aerial vehicles (UAV), commonly known as drones, have emerged as a rapidly evolving field with immense potential across diverse applications. A crucial aspect of UAV development is the method of launch, as it directly impacts the overall system design, efficiency, cost, and operational conditions. With the continuous introduction of …

Aerospace vehiclesThe use of suborbital launch vehicles for solutions in the field of safety and defense

The use of suborbital launch vehicles for solutions in the field of safety and defense

The use of suborbital launch vehicles for solutions in the field of safety and defense Vladyslav Proroka ORCID: https://orcid.org/0000-0001-6884-3934 Oles Honchar Dnipro National University Mykola Dron ORCID: https://orcid.org/0000-0003-0682-8004 Oles Honchar Dnipro National University Illia Lukianenko ORCID: https://orcid.org/0009-0004-4128-4377 Oles Honchar Dnipro National University Oleksii Kulyk ORCID: https://orcid.org/0000-0002-2913-4462 Oles Honchar Dnipro National University Suborbital launch vehicles and military rockets belong to separate classes of aerial vehicles that address different tasks and require distinct design approaches. The construction of suborbital launch vehicles is …

Aerospace vehiclesComparison of a combined torus tank with a composite isogrid support with existing design solutions

Comparison of a combined torus tank with a composite isogrid support with existing design solutions

Comparison of a combined torus tank with a composite isogrid support with existing design solutions Andrii Diadiuk ORCID: https://orcid.org/0009-0001-6923-3756 Oles Honchar Dnipro National University Volodymyr Lipovskyi ORCID: https://orcid.org/0000-0002-7939-7973 Oles Honchar Dnipro National University The development of spacecraft manufacturing technologies has made it possible to create improved designs. In this article, we study the design elements of the combined torus tank. A review of torus tank structures used in launch vehicles that have completed their missions shows that all of them …