Search Results for “Osinovyy H. H.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Mon, 09 Mar 2026 00:50:37 +0000 en-GB hourly 1 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “Osinovyy H. H.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 8.2.2025 Specificity of spaceport construction at a lunar base https://journal.yuzhnoye.com/content_2025_2-en/annot_8_2_2025-en/ Tue, 27 Jan 2026 08:54:29 +0000 https://journal.yuzhnoye.com/?page_id=35837
, Osinovyy H. ORCID , Osinovyy H. A., Osinovyy H. A., Osinovyy H. A., Osinovyy H. A., Osinovyy H. A., Osinovyy H. A., Osinovyy H.
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8. Specificity of spaceport construction at a lunar base

Date of receipt of the article for publication: 19.10.2025

Date of acceptance of the article for publication after review: 03.11.2025

Date of publication: 27.01.2026

e-ISSN: 2617-5533

ORCID authors:

Pustovharov A. A. ORCID, Husarova I. O. ORCID, Kozis K. V. ORCID, Lysenko Ya. A. ORCID, Osinovyy H. H. ORCID

Organization:

Yangel Yuzhnoye State Design Office

Page: Kosm. teh. Raket. vooruž. 2025 (2); 71-78

DOI: https://doi.org/10.33136/stma2025.02.071

Language: Ukrainian

Annotation: The 21st century started with changes in hopes and expectations for space exploration. Plans are being announced to move from researching and studying the solar system to colonizing it. The primary object of attention is the Earth’s natural satellite. A return to the Moon is expected in the near future, and various countries are already planning short-term crewed expeditions to the Moon. A gradual establishment of permanent human presence on the Moon is supposed, for which lunar bases will be created. One of the most essential tasks in exploring the Moon will be to ensure the reliable transportation of people and cargo between Earth and the Moon. The intensity of spacecraft fl ights will increase signifi cantly after the start of lunar base construction, remaining high in subsequent stages. Therefore, it can be expected that spaceports will become essential components of lunar bases. In addition to prepared sites, spaceports must have the necessary equipment and resources. The creation of a spaceport on the Moon has its own peculiarities, which are discussed in this article. The article examines the specifi city of spaceport construction on the Moon, considering the unusual nature of this task, and makes a brief analysis of modern approaches to accomplishing it. The article supposes the potential location of the spaceport, outlines the possible impact of lunar surface relief on spaceport construction, and identifi es factors of priority concern. The fi rst approximation provides the principal quantitative and qualitative indicators characterizing the spacecraft landing process. Recommendations are given regarding selecting the shape and size of landing pads for spacecraft. A possible structural diagram of a lunar spaceport has been developed, with a list of the primary components and equipment. The article also identifi es limitations that need to be taken into account and indicates various factors that will infl uence the design of the spaceport and, therefore, need to be considered. The work carried out may serve as a theoretical basis for the further development of the lunar base concept.

Key words: colonization of the Moon, lunar base, lunar spaceport, landing pad

Bibliography:

1. Artemis Plan. NASA’s Lunar Exploration Program Overview. September, 2020. 74 p. URL: https://nasa.gov/wp-content/uploads/2020/12/artemis_plan-20200921.pdf
2. Voelcker Ana Carolina. Moon base ad lunam. KTH Royal Institute of Technology. Stockholm, Sweden, 2023. 51 p. URL: https://www.diva-portal.org/smash/get/diva2:1868224/FULLTEXT01.pdf
3. Kysluk V. S. Kosmichni doslidzhennia Misiatsia: suchasnyi stan ta perspektyvy (ohliad). Kosmichna nauka i tekhnolohiia. 2013. T. 19. № 3. S. 5 – 20.
4. Melodie Yashar. ICON’s Project Olympus: Lunar Landing Pad Concept Design. URL: https://www.melodieyashar.com/lunar-landing-pad.html (data zvernennia 21.09.2025).
5. SpaceX Starship at NASA Artemis Base Camp by ICON. https://www.humanmars.net/search/label/Artemis%20Base%20Camp (data zvernennia 21.09.2025).
6. David L. How can we build landing and launch pads on the moon? 2024 https://www.space.com/the-moon-building-lunar-landing-launch-sites.
7. Kyryluk S. M. Pryroda Misiatsia: monohrafiia. Chernivtsi: Chernivetskyi nats. un-t im. Yuriia Fedkovycha, 2021. 240 s.
8. Kyryluk S. M. Landshaftni kompleksy malykh misiachnykh krateriv. Nauk. visn. Chernivetskoho universytetu: Zb. nauk. prats. Vyp. 633 – 634. Heohrafiia.
9. Kyryluk S. M., Spatar K. I. Heoloho-heomorfolohichni struktury vydymoi pivkuli Misiatsia. Nauk. visn. Chernivetskoho universytetu: Zb. nauk. prats. Vyp. 616. Heohrafiia. S. 101 – 112.
10. Stoyan Yu. G., Gil’ N. I. Metody’ i algoritmy’ razmeshheniya ploskix geometricheskix ob’’ektov. K.: Nauk. dumka, 1976. 249 s.

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2.1.2025 Justification of the parameters of a vertical screw conveyor for transporting lunar regolith https://journal.yuzhnoye.com/content_2025_1-en/annot_2_1_2025-en/ Wed, 27 Aug 2025 12:20:10 +0000 https://journal.yuzhnoye.com/?page_id=35479
Justification of the parameters of a vertical screw conveyor for transporting lunar regolith e-ISSN: 2617-5533 Authors: Semenenko Ye. G., Osinovyy G. Doslidzhennia travmuvannia zerna hvyntovym konveierom. Konstruiuvannia, vyrobnytstvo ta ekspluatatsia silskohospodarskykh mashyn. https://doi.org/10.3233/EPL-46204 18. V., Tokarchuk O. Osoblyvosti roboty krutopokhylenykh hvyntovykh transporteriv pry peremishchenni zernovoi produktsii. Tekhnika, enerhetyka, transport. Bulkhakov B. M., Adamchuk V. T., Trokhaniak O. Teoretychne obgruntuvannia parametriv hnuchkoho hvyntovoho konveiera dlia transportuvannia zernovykh materialiv. Visnyk ahrarnoi nauki.
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2. Justification of the parameters of a vertical screw conveyor for transporting lunar regolith

e-ISSN: 2617-5533

Organization:

National Academy of Sciences of Ukraine, M. S. Poliakov Institute of geotechnical mechanics2, Yangel Yuzhnoye State Design Office, Dnipro, Ukraine1

Page: Kosm. teh. Raket. vooruž. 2025 (1); 11-18

DOI: https://doi.org/10.33136/stma2025.01.011

Language: Ukrainian

Annotation: This paper aims to develop a scientifi cally grounded method for determining the key technical parameters of a vertical screw conveyor–specifi cally, throughput and the power requirement of the driving electric motor. These parameters depend on the density and porosity of the transported material, the screw’s geometric characteristics, and the gravitational fi eld at the transportation site. The study also explores potential design constraints when handling lunar regolith. To achieve this objective, the authors applied established equations for screw conveyor parameter calculations, fundamental principles of bulk material mechanics, key electrodynamic equations for asynchronous motors, and specifi c behavioral characteristics of bulk materials during vertical screw transport, which were also investigated experimentally. As a result, a novel method is proposed for calculating the technical specifi cations of a screw conveyor under lunar conditions, based on known geometric parameters, fi lling ratio, and electric motor characteristics. The study further examines the infl uence of the conveyor’s fi lling ratio on performance and identifi es geometric limitations imposed by the operational boundaries of the selected motor. Acceptable values for transport height, screw diameter, other geometric parameters, and achievable fi lling ratios for a given motor are determined. The study substantiates that vertical screw conveyors are the most promising solution for lunar regolith transport. These systems are compact, adaptable, capable of integration within tubes or underground installations, operate continuously, function autonomously, and can be powered by solar energy.

Key words: Moon, regolith, screw conveyor, electric motor, throughput, power

Bibliography:

1. Semеnenko Ye. V., Osadchaia N. V. Traditsionnyie i netraditsionnyie vidy energii, a takzhe kosmicheskiie poleznyie iskopaiemyie v okolozemnom prostranstve.
Nauchno-prakticheskaia konferentsiia «Sovremennyie raschetno-eksperimentalnyie metody opredeleniia kharakteristik raketno-kosmicheskoi techniki». m. Dnipro, 10 12 hrudnia 2019 r. S. 62 – 63. https://doi.org/10.1016/j.repl.2019.01.038

2. Jolliff B. L., Wieczorek M. A., Shearer C. K., Neal C. R. New Views of the Moon. Reviews in mineralogy and geochemistry. 2006. Vol. 60. 721 p. DOI: https://doi.org/10.2138/rmg.2006.60.0

3. Robert E. Grimm. Geophysical constaints on the lunar Procellarum KREEP Terrane. Journal of Geophysical Research: Planets. 2013. Vol. 118, Issue 4. P. 768-778. URL: https://agupubs-onlinelibrary-wiley-com.translate. goog/doi/10.1029/2012JE004114?_x_tr_sl=en&_x_tr_tl=ru&_x_tr_hl=ru&_x_tr_pto=sc
https://doi.org/10.1029/2012JE004114

4. Moon Village Association. URL: https://moon-villageassociation.org/about/

5. GLOBAL MOON VILLAGE. URL: https://space-architect.org/portfolio-item/ global-moon-village

6. Pustovharov А. А., Osynovyy G. G. Kontseptsiia shluzovogo modulia misiachnoi bazy. ХХV Mizhnarodna molodizhna naukovo-praktychna konferentsiia «Ludyna i kosmos».
Zbirnyk tez, NTSAOM, Dnipro, 2023. S. 86 – 87.

7. Berdnik A. I., Kaliapin M. D., Lysenko Yu. A., Bugaienko T. K. Mnogorazovyi lunnyi lender. Kosmichna nauka i technologiia. 2019. T. 25. № 5. S. 3-10.
https://doi.org/10.15407/knit2019.05.003

8. Semenenko P. V. , Groshelev D. G., Osinovyy G. G., Semenenko Ye. V., Osadchaia N. V. Sposoby transportirovki poleznykh iskopaiemykh ot mesta ikh dobychi k mestu pererabotki v lunnykh usloviiakh. XVII konferentsiia molodykh vchenykh «Heotekhnichni problemy rozrobky rodovyshch». m. Dnipro, 24 zhovtnia 2019 r. S 7.

9. Komatsu pobuduie ekskavator dlia roboty na Misiatsi. URL: https://www.autocentre.ua/ua/ news/concept/komatsu-postroit-ekskavator-dlya-raboty-na-lune-1380272.html.

10. Help NASA Design a Robot to Dig on the Moon. URL: https://www.nasa.gov/directorates/ stmd/help-nasa-design-a-robot-to-dig-on-the-moon/

11. Semenenko Ye. V. , Semenenko P. V., Hroshelev D. H. Tekhnolohichni parametry shneka dlia transportuvannia misiachnoho reholitu. Zbirka tez ХХVІ Mizhnarodnoi molodizhnoi naukovo-praktychnoi konferentsii «Ludyna i kosmos», Dnipro, 17 – 19 kvitnia, 2024. S. 132 – 133.

12. Semenenko Ye. V. , Biliaiev M. M., Semenenko P. V. Rozrakhunok parametriv systemy transportuvannia misiachnogo reholitu. Space Technology. Missile Armaments. Zb.
nauk.-tekhn. st. 2024. Vyp. 1. Dnipro: DP «KB «Pivdenne». S. 93 – 101.
https://doi.org/10.33136/stma2024.01.093

13. Bezruchko K. A. Review of potential sources for obtaining energy carriers and mineral raw materials in outer space. Heotekhnichna mekhanika. 2022. № 163. S.140-154. https://doi.org/10.15407/geotm2022.163.140

14. Nouman Khan, Muhammad Kaleem Sarwar, Muhammad Rashid, Hafiz Kamran Jalil Abbasi, Saif Haider, Muhammad Atiq Ur Rehman Tariq, Abdullah Nadeem, Muhammad Ahmad
Zulfiqar, Ali Salem, Nadhir Al-Ansari, Abdelaziz M. Okasha, Ahmed Z. Dewidar&Mohamed A. Mattar. Development of a sustainable portable Archimedes screw turbine for hydropower generation. Scientific Reports. 2025. Vol. 15. Issue 1. DOI
https://doi.org/10.1038/s41598-025-90634-8

15. Kumar Thakur N., Thakur R., Kashyap K., Goel B. Efficiency enhancement in Archimedes screw turbine by varying different input parameters – An experimental study.
Materials Today: Proceedings. 2022. Vol. 52, Part 3. P. 1161-1167.
https://doi.org/10.1016/j.matpr.2021.11.020

16. Kozyn A., Lubitz W. D. A power loss model for Archimedes screw generators. Renewable Energy. 2017, Vol. 108. P. 260-273.
https://doi.org/10.1016/j.renene.2017.02.062

17. Kulykivskii V. L., Paliichuk V. K., Borovskyi V. M. Doslidzhennia travmuvannia zerna hvyntovym konveierom. Konstruiuvannia, vyrobnytstvo ta ekspluatatsia silskohospodarskykh mashyn. 2016. Vyp. 46. S. 160-165.
https://doi.org/10.3233/EPL-46204

18. Lubin M. V., Tokarchuk O. A., Yaropud V. M. Osoblyvosti roboty krutopokhylenykh hvyntovykh transporteriv pry peremishchenni zernovoi produktsii. Tekhnika, enerhetyka, transport. APK. 216. № 3 (95). S. 235-240.

19. Bulkhakov B. M., Adamchuk V. V., Nadykto V. T., Trokhaniak O. M. Teoretychne obgruntuvannia parametriv hnuchkoho hvyntovoho konveiera dlia transportuvannia zernovykh materialiv. Visnyk ahrarnoi nauki. 2023. № 4 (841). S. 59 – 66.

20. Semenenko Ye. V. Nauchnyie osnovy tekhnologii gidromekhanizatsii otkrytoi razrabotki titan-tsyrkonovykh rossypei. Kiev: Naukova dumka, 2011. 232 s.

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