Search Results for “lunar base” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Mon, 16 Mar 2026 14:04:39 +0000 en-GB hourly 1 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “lunar base” – 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
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 ISSN: 2617-5525 e-ISSN: 2617-5533 Authors: Pustovharov A. quot;Specificity of spaceport construction at a lunar base," Космическая техника. quot;Specificity of spaceport construction at a lunar base," Космическая техника. H., Specificity of spaceport construction at a lunar base, Космическая техника. Specificity of spaceport construction at a lunar base. Specificity of spaceport construction at a lunar base. (2026) Specificity of spaceport construction at a lunar base, Космическая техника. "Specificity of spaceport construction at a lunar base." Космическая техника. Specificity of spaceport construction at a lunar base. Specificity of spaceport construction at a lunar base.
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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

ISSN: 2617-5525

e-ISSN: 2617-5533

Authors:

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

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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]]> 7.2.2025 Autonomous deployable landing interface: a detailed technical framework for Mitigating terminal descent risks on planetary surfaces https://journal.yuzhnoye.com/content_2025_2-en/annot_7_2_2025-en/ Tue, 27 Jan 2026 08:45:39 +0000 https://journal.yuzhnoye.com/?page_id=35834
This paper presents a detailed technical framework for the Lunar Landing Interface (LLI), a deployable, autonomous ground structure designed to create a controlled environment that mitigates these universal risks. The scientifi c novelty of this work lies in the integrated systems approach, combining origami-inspired deployment with active dust mitigation and ground-based autonomous guidance to solve the terminal descent problem holistically. The practical signifi cance is a clear path toward reducing the cost and increasing the safety of lunar access, thereby enabling a sustainable lunar economy. Intuitive machines’ private athena probe lands near lunar south pole – but it may have tipped over, 20.
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7. Autonomous deployable landing interface: a detailed technical framework for Mitigating terminal descent risks on planetary surfaces

Date of receipt of the article for publication: 03.11.2025

Date of acceptance of the article for publication after review: 17.11.2025

Date of publication: 27.01.2026

ISSN: 2617-5525

e-ISSN: 2617-5533

Автори: Iteba A. K., Weramundi N. E.

Organization: University of Nairobi

Page: Kosm. teh. Raket. vooruž. 2025 (2); 67-70

DOI: https://doi.org/10.33136/stma2025.02.067

Language: English

Annotation: The terminal descent phase of landing is a mission-critical failure point for all planetary surface exploration. This paper presents a detailed technical framework for the Lunar Landing Interface (LLI), a deployable, autonomous ground structure designed to create a controlled environment that mitigates these universal risks. We provide an in-depth analysis of the material science, component design, and operational principles of the LLI. Specifi c focus is given to the proposed solutions for electromagnetic compatibility (EMC); the power nfrastructure required for high-voltage electrostatic systems; the system’s structural and mechanical reliability through the use of solid-state actuators and robust materials; and the strategic costbenefi t of lander mass reduction enabled by this infrastructure. The scientifi c novelty of this work lies in the integrated systems approach, combining origami-inspired deployment with active dust mitigation and ground-based autonomous guidance to solve the terminal descent problem holistically. The practical signifi cance is a clear path toward reducing the cost and increasing the safety of lunar access, thereby enabling a sustainable lunar economy. This work expands upon a preliminary concept to provide the detailed theoretical and engineering rationale necessary to prove the LLI’s feasibility and justify further investment in its development, directly addressing reviewer feedback

Key words: Lunar Landing, Terminal Descent, Dust Mitigation, Origami Structures, Autonomous Systems, Spacecraft Design, Regolith, ShapeMemory Alloys

Bibliography:

1. Mike Wall. Intuitive machines’ private athena probe lands near lunar south pole – but it may have tipped over, 20.
2. NASA Science. Beresheet, 2019.
3. KYODO NEWS. Japan ispace fails in bid for 1 st moon landing by asian private firm, 2025.
4. Thornton Bryce, Ireland Tom. The economics of reusable launch vechicles. New Space. 10(2). 125-135, 2022.
5. Attard M., Chirima G., Kar-Eng K. A review of the applications of indium tin oxide (ito). Journal of Physics: Conference Series, 2071:012001, 2021.
6. Shaw J.A., Grummon D.S., Folias S. Shape memory alloy applications in aerospace. Progress in Aerospace Sciences, 126:100743, 2021.
7. Sternovsky Z., Szalay J.R., Horányi M., Drake E. Photoelectric charding and transport of lunar dust. Journal of Geophysical Research: Planets. 128 (5), 2023.

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]]> 1.1.2025 Promomoon initiative for moon village generation in honor of dr. Alexander degtyarev https://journal.yuzhnoye.com/content_2025_1-en/annot_1_1_2025-en/ Sun, 25 Jan 2026 23:53:07 +0000 https://journal.yuzhnoye.com/?page_id=35475
Most of the projects are dedicated to the creation of lunar base infrastructure and technologies for extracting useful resources on the Moon. The modules are made of terrestrial materials, lunar regolith, and a building material based on radiation-absorbing fungi, as well as “PotatoCreteˮ material derived from potato raw materials. The Lunar-Based Solar Power Station with Microwave Power Transmission from a Satellite Orbiter was developed by the Lunar Energizers team, and the Lunar Regolith-Based ThermalEnergy Storage for Moon Village Generation, in the project of the same name. Project Lunar-based Solar Power Station with Microwave Power Transmission Satellite Orbiter.
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1. Promomoon initiative for moon village generation in honor of dr. Alexander degtyarev

ISSN: 2617-5525

e-ISSN: 2617-5533

Автори: Degtiarov M. O., Gusarova I. O., Osynovyy G. G.

Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2025 (1); 3-10

DOI: https://doi.org/10.33136/stma2025.01.003

Language: English

Annotation: Moon Village Association, together with Yuzhnoye State Design Offi ce, created and implemented the Mentorship Program “PromoMoon Initiative for Moon Village Generation in honor of Dr. Alexander Degtyarev ˮ. The main goal of the Program is to build the capacity of new participants in the space market. The Mentorship Program allows the winners of the competition to receive expert assessment through online B2B mentorship sessions provided by MVA members and specialists from Yuzhnoye State Design Offi ce. This year marks the 4th PromoMoon Initiative. 19 projects are presented by participants from 16 countries. Most of the projects are dedicated to the creation of lunar base infrastructure and technologies for extracting useful resources on the Moon. The main focus of the proposed projects is on the use of local resources, cost-eff ectiveness and reliability. Seven projects are dedicated to various residential module designs: with an infl atable chamber and high-strength shells; with small 3D-printed panels and their assembly in a module; modular habitats created and serviced by autonomous microrobots; modules using biomimetic principles of adaptation found in Earth’s natural systems. The modules are made of terrestrial materials, lunar regolith, and a building material based on radiation-absorbing fungi, as well as “PotatoCreteˮ material derived from potato raw materials. The Lunar-Based Solar Power Station with Microwave Power Transmission from a Satellite Orbiter was developed by the Lunar Energizers team, and the Lunar Regolith-Based ThermalEnergy Storage for Moon Village Generation, in the project of the same name. The Tochtli system for regolith extraction and processing was proposed by the Torres Orbital Mining team, the RegOne system for regolith extraction and transportation was proposed by the MoonAixperts e.V. team. Anodes for direct molten regolith electrolysis were developed by a team of Ukrainian scientists. The Sand to Green team developed a lunar agroforestry system. Two launch complexes, the Lunar Electrostatic Dust Removal Station, a lunar rescue sled and a centralized cloud platform with open access for storing, analyzing and exchanging lunar mission data were proposed.

Key words: lunar modules, local resources, extraction of useful resources

Bibliography:

1. Project Oxygen Space. URL: https://moonvillageassociation.org/announcement-4th-promomoon-intiative.

2. Project Moon Arc / M.S.C.A.P.E. URL: https://moonvillageassociation.org/ announcement-4th-promomoon-intiative.

3. Project Lunar Metropolis: 3D-Printed Modular Habitat. URL: https://moonvillageassociation.org/ announcement-4th-promomoon-intiative.

4. Project Pine flex lunar biome. URL: https://moonvillageassociation.org/ announcement-4th-promomoon-intiative.

5. Project Lunar-based Solar Power Station with Microwave Power Transmission Satellite Orbiter. URL: https://moonvillageassociation.org/ announcement-4th-promomoon-
intiative.

6. Project TOM’s Tochtli and Lunar regolith excavation. URL: https://moonvillageassociation.org/ announcement-4th-promomoon-intiative.

7. Project URL: https://moonvillageassociation.org/ announcement-4th-promomoon-intiative.

8. O.N. Grigoriev, I.P. Neshpor, T.V. Mosina, V.B. Vinokurov, A.V. Koroteev, O.V. Buriachek, D.V. Vedel, A.N. Stepanchuk, L. Silvestroni, Behavior of Ultrahigh
Temperature ZrB2-Based Ceramics in Oxidation. Powder Metallurgy and Metal Ceramics. 2018. № 56.573-580 р. DOI: https://doi.org/10.1007/s11106-018-9930

9. D.Vedel, O.Grigoriev, P.Mazur, A.Osipov, M.Brodnikovskyi, L.Silvestroni, Effect of Mo2C addition on the mechanical properties and oxidation resistance of ZrB2-SiC
ceramics. Journal of Alloys and Compounds. 2021. V. 879. P. 160398 DOI: https://doi.org/10.1016/j.jallcom.2021.160398.

10. Gusarova I. O., Lysenko Yu. O., Osinovyy G.G., Future projects of lunar exploration implemented by Yuzhnoye SDO. Space technology. Missile armaments, 2024, № 1
(121). P. 19-28. https://doi.org/10.33136/stma2024.01.019

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]]> 6.1.2025 Studying the landing of the reusable first stage of the Cyclone-5 space launch vehicle on a maritime landing platform-duplicate-1 https://journal.yuzhnoye.com/content_2025_1-en/annot_6_1_2025-en/ Wed, 27 Aug 2025 13:43:20 +0000 https://journal.yuzhnoye.com/?page_id=35488
Overcoming these technical challenges would enable the creation of an autonomous lunar resource extraction system, which is critical for future lunar bases and further space exploration.
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6. Mining on the Moon

ISSN: 2617-5525

e-ISSN: 2617-5533

Автори: Gusarova I. O., Kozis K. V, Osinovyy G. G.

Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2025 (1); 45-51

DOI: https://doi.org/10.33136/stma2025.01.045

Language: English

Annotation: Modern research into technologies for extracting mineral resources on the Moon has revealed some harsh limitations related to dependence on Earth’s resources and high technological requirements. While the chemical and carbothermal reduction of lunar regolith is theoretically possible, it requires a constant supply of reducing agents such as hydrogen or carbon from Earth. This signifi cantly increases mission costs and complicates logistics, making such methods unsuitable for large-scale applications. Pyrolysis, which involves heating regolith to extremely high temperatures, is also not an optimal solution due to the need for complex and energy-intensive equipment that exceeds the capabilities of current space technologies. Electrolysis using molten fl uoride salts or calcium chloride (CaCl2 ) has been proposed as an alternative, but its effi ciency is limited by the need to deliver fl uxes from Earth. This reduces the autonomy of the process and makes it less economically viable in the long term. In light of these limitations, the most promising technology appears to be the direct electrolysis of molten regolith, which stands out for its simplicity and independence from terrestrial materials. This method involves melting local raw materials, followed by electrolytic separation into useable components such as oxygen, metal alloys, and other materials. However, the key challenge to implementing this technology is the development of refractory conductive materials for anodes that can withstand the extreme conditions of high temperatures and aggressive oxygen environments. Existing materials degrade rapidly under these factors, leading to reduced effi ciency and increased maintenance costs. Additionally, reliable protective coatings for equipment must be developed to prevent corrosion and mechanical wear. Overcoming these technical challenges would enable the creation of an autonomous lunar resource extraction system, which is critical for future lunar bases and further space exploration. Such a system could provide astronauts with oxygen, water, and construction materials without constant supplies from Earth, signifi cantly reducing the cost of space missions. Thus, despite existing technological challenges, direct electrolysis remains the most viable option for the industrial use of local lunar resources. Further research should focus on optimizing materials and application methods, as well as on developing energy-effi cient solutions to ensure the stability and economic feasibility of lunar mining. This will open new possibilities for a sustained human presence on the Moon and will be a signifi cant step in deep space exploration.

Key words: Electrochemical reduction of melts, inert anodes, electrolysis, pyrolysis

Bibliography:

1. NEEP602 Course Notes (Fall 1996) Resources from Space. URL: https://fti.neep.wisc.edu/fti.neep.wisc.edu/neep602/lecture12.html.

2. Lunarpedia. Ilmenite Reduction. URL: https://lunarpedia.org/w/Ilmenite_Reduction.

3. S. J. Barber et al. ProSPA: Analysis of Lunar Polar Volatiles and ISRU Demonstration on the Moon. 49th Lunar and Planetary Science Conference 2018 (LPI Contrib. No.
2083). URL: https://www.cosmos.esa.int/documents/1568476/1766000/RD5_2018_LPSC_ PROSPECT_ProSPA_Poster_Abstract2172.pdf

4. Oxygen on the Moon. Oxygen production in the Moon extended summary. URL: https://www.ou.edu/class/che-design/a-design/projects-2004/Oxygen-Production-in-the-Moon-
Extended-Summary.pdf.

5. The Moon’s top layer alone has enough oxygen to sustain 8 billion people for 100,000 years. URL: https://theconversation-com./the-moons-top-layer-alone-has-enough-
oxygen-to-sustain-8-billion-people-for-100-000-years.

6. From lunar regolith to oxygen and structural materials: an integrated conceptual design. URL: https://link.springer.com/article/10.1007/s12567-022-00465-w.

7. Proving the viability of an electrochemical process for the simultaneous extraction of oxygen and production of metal alloys from lunar regolith. URL:
https://pure.hw.ac.uk/ws/portalfiles/portal. Lomax, BA, Conti, M, Khan, N, Bennett, NS, Ganin, AY & Symes, MD 2019. Proving the viability of an electrochemical process
for the simultaneous extraction of oxygen and production of metal alloys from lunar regolith, Planetary and Space Science. https://doi.org/10.1016/j.pss.2019.104748.

8. L. Glaze, Moon’s South Pole in NASA’s Landing Sites, NASA. (2019). URL: https://www.nasa.gov/feature/moon-s-south-pole-in-nasa-s-landing-sites.

9. Feasibility Analysis of Liquefying Oxygen Generated from Water Electrolysis Units on Lunar Surface. URL: https://ntrs.nasa.gov/citations/20100020908, Feasibility
Analysis of Liquefying Oxygen Generated from Water Electrolysis Units on Lunar Surface.

10. Moon oxygen startup stumbles on ‘green’ iron production-method. URL: https://www.israelhayom.com/2022/07/17/moon-oxygen-startup-stumbles-on-green-iron-production-
method.

11. Eric Berger. Machine to melt Moon rocks and derive metals may launch in 2024. URL: https://arstechnica.com/science/2022/01/machine-to-melt-moon-rocks-and-derive-
metals-may-launch-in-2024.

12. Hydrogen-oxygen proton-exchange membrane fuel cells and electrolyzers. URL: https://www.science.gov/topicpages/e/electrolyzer+component+development.

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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
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.
]]>

2. Justification of the parameters of a vertical screw conveyor for transporting lunar regolith

ISSN: 2617-5525

e-ISSN: 2617-5533

Authors:

Semenenko Ye. V.2, Semenenco P. V.1

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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]]> 11.1.2024 PARAMETERS CALCULATION OF THE LUNAR REGOLITH TRANSPORT SYSTEM https://journal.yuzhnoye.com/content_2024_1-en/annot_11_1_2024-en/ Mon, 17 Jun 2024 08:41:21 +0000 https://journal.yuzhnoye.com/?page_id=35014
It has been proven that the solutions based on using auger conveyors would be most rational for transporting loose lunar regolith over the Moon’s surface because the auger conveyors are compact and adaptable, and they can be placed inside tubes and laid under the day surface, thereby ensuring the continuous transportation process.
]]>

11. Parameters calculation of the lunar regolith transport system

ISSN: 2617-5525

e-ISSN: 2617-5533

Authors:

Semenenko Ye. V.1, Biliaiev M. M.2, Semenenko P. V.3

Organization:

National Academy of Sciences of Ukraine, M.S. Poliakov Institute of geotechnical mechanics1; Ukrainian State University of Science and Technologies2; Yangel Yuzhnoye State Design Office, Dnipro, Ukraine3

Page: Kosm. teh. Raket. vooruž. 2024, (1); 93-101

DOI: https://doi.org/10.33136/stma2024.01.093

Language: Ukrainian

Annotation: The objective of this article is to develop a scientifically proven method of calculation of the auger conveyor parameters, such as the conveyor capacity and the corresponding power of the electrical motor, for different densities and porosities of conveyed materials, the geometrical parameters of the auger, and the specificity of the gravitational fields at the place of transportation. Another objective is to investigate potential limitations of the auger parameters when transporting lunar regolith. To reach these objectives, the known relations for calculating the auger conveyor parameters were applied, as well as the fundamental laws of the granular media mechanics, the principal equations of asynchronous motor electrodynamics, and the behavior of granular media when moving it with the auger conveyor, experimentally studied by the domestic authors. It gave the possibility, for the first time for the lunar environment, to suggest a procedure to calculate the auger conveyor parameters, such as the conveyor capacity and the corresponding power of the electric motor, using known geometrical parameters of the mainline and pipeline, the auger conveyor filling ratio and the parameters of the selected electrical motor. It gave the possibilities to study how the filling ratio of the auger conveyor influences its principal performance parameters and determine potential limitations of the geometrical parameters and the filling ratios of auger conveyors according to the parameters and features of the selected electrical motor. The allowable transportation distances, diameters, other geometrical parameters of auger conveyors, and conveyor filling ratios with the selected electrical motor have been determined. It has been proven that the solutions based on using auger conveyors would be most rational for transporting loose lunar regolith over the Moon’s surface because the auger conveyors are compact and adaptable, and they can be placed inside tubes and laid under the day surface, thereby ensuring the continuous transportation process. Furthermore, they are capable of autonomous operation and can use the electricity produced by solar arrays.

Key words: Moon, regolith, auger, electric motor, capacity, power

Bibliography:

1. Pustovgarov A. A., Osinoviy G. G. Kontseptsiya shlyuzovogo modulya misyachnoi bazy. ХХV Mizhnarodna molodizhna naukovo-praktychna conf. «Lyudyna i cosmos». Zbirnyk tez, NTsAOM, Dnipro, 2023. S. 86 – 87.
2. Semenenko P. V. Sposoby transortirovki poleznykh iskopaemykh ot mesta ikh dobychi k mestu pererabotki v lunnykh usloviyukh. P. V. Semenenko, D. G. Groshelev, G. G. Osinoviy, Ye. V. Semenenko, N. V. Osadchaya. XVII conf. molodykh vchenykh «Geotechnichni problemy rozrobky rodovysch». m. Dnipro, 24 zhovtnya 2019 r. S. 7.
3. Berdnik A. I. Mnogorazoviy lunniy lander. A. I. Berdnyk, M. D. Kalyapin, Yu. A. Lysenko, T. K. Bugaenko. Raketno-kosmichny complexy. 2019. T. 25. №5:3-10. ISSN 1561-8889. https://doi.org/10.15407/knit2019.05.003
4. Semenenko Ye. V., Osadchaya N. V. Traditsionnye i netraditsionnye vydy energii, a takzhe kosmicheskie poleznye iskopaemye v okolozemnom prostranstve. Nauch.-parakt. conf. «Sovremennye raschetno-experimentalnye metody opredeleniya characteristic raketno-kosmicheskoy techniki». m. Dnipro, 10 – 12 grudnya 2019 r. S. 62 – 63.
5. Komatsu pobudue excavator dlya roboty na Misyatsi https://www.autocentre.ua/ua/ news/concept/komatsu-postroit-ekskavator-dlya-raboty-na-lune-1380272.html.
6. Help NASA Design a Robot to Dig on the Moon https://www.nasa.gov/directorates/ stmd/help-nasa-design-a-robot-to-dig-on-the-moon/
7. Robert E. Grimm. Geophysical constaints on the lunar Procellarum KREEP Terrane. Vol. 118, Issue 4. April 2013. P. 768-778. 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
8. Chen Li. A novel strategy to extract lunar mare KREEP-rich metal resources using a silicon collector. Kuixian Wei, Yang Li, Wenhui Ma, Yun Lei, Han Yu, Jianzhong Liu. Journal of Rare Earths Vol. 41, Issue 9, September 2023, P. 1429-1436. https://www-sciencedirect-com.translate.goog/science/article/ abs/pii/S1002072122001910?_x_tr_sl=en&_x_tr_tl=ru&_x_tr_hl=ru&_x_tr_pto=sc https://doi. org/10.1016/j.jre.2022.07.002
9. Moon Village Association https://moon-villageassociation.org/about/
10. GLOBAL MOON VILLAGE. https://space-architect.org/portfolio-item/ global-moon-village//
11. Just G. H. Parametric review of existing regolith excavation techniques for lunar In Situ Resource Utilization (ISRU) and recommendations for future excavation experiments. G. H. Just, Smith K., Joy K. H., Roy M. J. https://doi.org/10.1016/j.pss.2019.104746
https://www.sciencedirect.com/science/article/pii/S003206331930162X
12. Anthony J. Analysis of Lunar Regolith Thermal Energy Storage. Anthony J. Colozza Sverdrup Technology, Inc. Lewis Research Center Group Brook Park, Ohio NASA Contractor Report 189073. November 1991. S-9 https://denning.atmos.colostate.edu/readings/ lunar.regolith.heat.transfer.pdf
13. Obgruntuvannya vykorystannya shneka dlya utilizatsii vidkhodiv vuglezbagachennya z mozhlyvistyu pidvyschennya bezpeki energetychnoi systemy pidpriemstv. SLobodyannikova I. L., Podolyak K. K., Tepla T. D. Materialy XХІ Mizhnarod. conf. molodykh vchennykh (26 zhovt. 2023 roku, m. Dnipro). Dnipro: IGTM im. M.S. Polyakova NAN Ukrainy, 2023. S. 50–55.
14. Kulikivskiy V. L., Paliychuk V. K., Borovskiy V. M. Doslidzhennya travmuvannya zerna gvintovym konveerom. Konstryuvannya, vyrobnitstvo ta exspluatatsiya silskogospodarskykh mashin. 2016. Vyp. 46. S. 160 – 165. https://doi.org/10.3233/EPL-46204
14. Lyubin M. V., Tokarchuk O. A., Yaropud V. M. Osoblyvosti roboty krutopokhylennykh gvyntovykh transporterov pri peremischenni zernovoi produktsii. Tekhnika, energetika, transport APK. 216. № 3(95). S. 235 – 240.
15. Gevko R. B., Vitroviy A. O., Pik A. I. Pidvyschennya tekhnichnogo rivnya gnuchkykh gvyntovykh konveeriv. Ternopil: Aston, 2012. 204 s.
16. Bulgakov B. M., Adamchyuk V. V., Nadikto V. T., Trokhanyak O. M. Teoretichne obgruntuvannya parametriv gnuchkogo gvintovogo konveera dlya transportuvannya zernovykh materialiv. Visnyk agrarnoi nauki. 2023. № 4(841). S. 59 – 66.
17. New Views of the moon. Reviews in mineralogy and geochemistry. Eds. Joliff B.L., Wieczorek M.A., Shearer C.K., Neal C.R. Mineralogical Society of America. Reviews in mineralogy and geochemistry. 2006. Vol. 60. 721 p. DOI: 10.2138/rmg.2006.60.
18. Semenenko Ye. V. Nauchnye osnovy technologiy hydromechanizatsii otkrytoy razrabotki titan-cyrkonovykh rossypey. Yevgeniy Vladimirovich Semenenko. Kiev: Nauk. dumka, 2011. 232 s.

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The influence of electric motor power on the parameters of the moon regolith extraction site
Pavlo Semenenko, Mykola Olehovych Pozdnyshev, Volodymyr Zaverukha et al. (2025)
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]]> 3.1.2024 Future projects of lunar exploration implemented by Yuzhnoye SDO https://journal.yuzhnoye.com/content_2024_1-en/annot_3_1_2024-en/ Wed, 12 Jun 2024 15:28:59 +0000 https://journal.yuzhnoye.com/?page_id=34965
2024, (1); 19-28 DOI: https://doi.org/10.33136/stma2024.01.019 Language: English Annotation: Over the past years, the leading space powers have been returning to the idea of expeditions to the Moon and actively designing and manufacturing components for inhabited lunar bases. Yuzhnoye State Design Office has its own concept of a lunar base and, of course, cannot stand aside from the solution of scientific and technical problems related to the Moon exploration. Based on the analysis of the Lunar Industrial & Research Base conceptual design, such technologies may include rocket propulsion, units and assemblies of liquid-propellant propulsion (TRL 6–9), as well as future designs such as a hydrogen energy accumulator and inert anodes made of ultra-high-temperature ceramics for electrolysis of regolith melts.
]]>

3. Future projects of lunar exploration implemented by Yuzhnoye SDO

ISSN: 2617-5525

e-ISSN: 2617-5533

Authors:

Husarova I. O., Lysenko Yu. O., Osinovyi G. G.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2024, (1); 19-28

DOI: https://doi.org/10.33136/stma2024.01.019

Language: English

Annotation: Over the past years, the leading space powers have been returning to the idea of expeditions to the Moon and actively designing and manufacturing components for inhabited lunar bases. Yuzhnoye State Design Office has its own concept of a lunar base and, of course, cannot stand aside from the solution of scientific and technical problems related to the Moon exploration. Specialists of Yuzhnoye SDO completed conceptual development of a significant range of technologies required for the Moon exploration: a space transportation system for lunar expeditions; landers to deliver payloads to the surface of the Moon and transport experimental equipment; mobile laboratories; a reconnaissance rover to provide reconnaissance missions on the surface of the Moon; vehicles to provide lifting and transport, assembly and construction, production and technological and soil extraction work on the surface of the Moon; habitat units and other elements of the lunar infrastructure. Taking into account the high costs of lunar exploration, it is clear that international cooperation is the most realistic scenario for Yuzhnoye SDO to participate in the exploration. The U.S. lunar program is the most attractive. Private companies that NASA selects for the lunar programs can become partners of Yuzhnoye. With a view to ensuring the participation of Yuzhnoye SDO in international programs, the current state of global technologies for the Moon exploration was analyzed and opportunities to promote technologies developed by Ukrainian specialists on the international market of space technologies were identified based on the analysis. Taking into account the high level of technologies developed by the potential partners, it is proposed for the first time to consider it advisable to promote Yuzhnoye’s technologies with TRL 6–9 which have already been successfully tested and the innovative technologies developed by the company which have no analogues in the world or surpass the world level in terms of their technological and economic performance. Based on the analysis of the Lunar Industrial & Research Base conceptual design, such technologies may include rocket propulsion, units and assemblies of liquid-propellant propulsion (TRL 6–9), as well as future designs such as a hydrogen energy accumulator and inert anodes made of ultra-high-temperature ceramics for electrolysis of regolith melts.

Key words: rocket propulsion, hydrogen energy accumulator, inert anodes.

Bibliography:
1. Rosiya vtratyla “Lunu-25”, India uspishno zavershyla misiu. Chomu krainy ponovyly gonku za resursy Misyatsa? 23 serpnya 2023. https://www.epravda.com.ua/publications/2023/08/23/703510 (Russia lost Luna-25, India successfully completed the mission. Why have countries renewed the race for lunar resources? August 23, 2023. In Ukrainian)
2. Creech S, Guidi J, Elburn D. Artemis: An overview of NASA’s activities to return humans to the Moon. Paper presented at: 2022 IEEE Aerospace Conference (AERO); 2022 Mar 05-12; Big Sky, Montana.
https://doi.org/10.1109/AERO53065.2022.9843277
3. In-Situ Resource Utilization (ISRU) Demonstration Mission, 2019. https://exploration.esa.int/web/moon/-/60127-in-situ-resource-utilisation-demonstration-mission.
4. Peng Zhang, Wei Dai, Ran Niu, Guang Zhang, +12 authors. Overview of the Lunar In Situ Resource Utilization Techniques for Future Lunar Missions. Journal Space: Science & Technology. 2023, Vol. 3, Р. 1-18. Article ID: 0037. DOI: 10.34133/space.0037
https://doi.org/10.34133/space.0037
5. Lin XU, Hui LI, Pei Z, Zou Y, Wang C. A brief introduction to the International Lunar Research Station Program and the Interstellar Express Mission. Chinese J Space Sci. 2022;42(4):511-513.
https://doi.org/10.11728/cjss2022.04.yg28
6. Li C, Wang C, Wei Y, Lin Y. China’s present and future lunar exploration program. Science. 2019;365(6450):238-239.
https://doi.org/10.1126/science.aax9908
7. Ukrinform, 09 sichnya 2024, https://www.ukrinform.ua/rubric-technology/3804665-aponskij-zond-uvijsov-do-orbiti-misaca-pered-posadkou.html (Ukrinform, January 9, 2024. In Ukrainian).
8. Nimechina priednalasya do programmy vyvchennya Misyatsa Artemis, 15.09.2023, https://www.dw.com/uk/nimeccina-priednalas-do-programi-vivcenna-misaca-artemis/a-66826693 (Germany joined the Artemis moon exploration program, September 15, 2023. In Ukrainian).
9. Grigoriev O. N., Frolov G. A., Evdokimenko Yu. I., Kisel’ V. M., Panasyuk A. D., Melakh L. M., Kotenko V. A., Koroteev A. V. Ultravysokotemperaturnaya keramika dlya aviatsionno-kosmicheskoy techniki, Aviatsionno-kosmicheskaya technika i technologiya, 2012, No 8 (95), st.119-128 (O.N. Grigoriev, G.A. Frolov, Yu.I. Evdokimenko, V.M. Kisel, A.D. Panasyuk, L.M. Melakh, V.A. Kotenko, A.V. Koroteev. Ultra-high-temperature ceramics for aerospace engineering, Aerospace engineering and technology, 2012, No. 8 (95), Р. 119-128. In Russian).
10. Grigoriev O. N. et al. Oxidation of ZrB2-SiC-ZrSi2 ceramics in oxygen. Journal of the European Ceramic Society 30 (2010). 2397-2405.
https://doi.org/10.1016/j.jeurceramsoc.2010.03.016

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]]> 1.2.2018 Design Office of Liquid Rocket Engines is 60 https://journal.yuzhnoye.com/content_2018_2-en/annot_1_2_2018-en/ Thu, 07 Sep 2023 08:19:39 +0000 https://journal.yuzhnoye.com/?page_id=30723
The required test benches and production base were created. Among them we should mention the RD858 and RD859 engines for the soviet lunar take-off-and –landing module of Block E, the unique RD857 and RD862 engines with afterburning of reducing generator gas and gas dynamic method of thrust vector control, the RD866 multifunctional engine of space tug ensuring multiple ignition in flight, and many others. Based on Yuzhnoye SDO–created engines, propulsions systems for ballistic missiles and space rockets that are unique by their characteristics and scope of functions, the engines, propulsions systems for spacecraft, LV upper stages and transfer orbit stages can be developed in short terms and at minimal costs. Possibilities of Creating New LRE Based on Mature Technologies.
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1. Design Office of Liquid Rocket Engines is 60

ISSN: 2617-5525

e-ISSN: 2617-5533

Authors:

Shulga V. A., Dibrivny O. V.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2018 (2); 3-7

DOI: https://doi.org/10.33136/stma2018.02.003

Language: Russian

Annotation: During 60 years of existence of specialized Liquid Rocket Engines Design Office – DO-4 as a part of Yuzhnoye Design Office, extensive experience was accumulated in development of liquid rocket engines of various purpose on storable and cryogenic propellant components. The required test benches and production base were created. When developing the engines, the DO-4 specialists widely use the experience accumulated during manufacturing and testing of the engines developed by the other design offices for Yuzhnoye SDO LVs that were manufactured by SE PA Yuzhny Machine-Building Plant and tested at Yuzhnoye SDO’s and Plant’s test benches. Along with the conventional ones, new original engine designs were developed to achieve high energy-mass characteristics, reliability and quality. Among them we should mention the RD858 and RD859 engines for the soviet lunar take-off-and –landing module of Block E, the unique RD857 and RD862 engines with afterburning of reducing generator gas and gas dynamic method of thrust vector control, the RD866 multifunctional engine of space tug ensuring multiple ignition in flight, and many others. At present, Yuzhnoye SDO jointly with SE PA Yuzhny Machine-Building Plant deliver the engine for the European Vega LV forth stage propulsion system under the contract with Avio company (Italy). Based on Yuzhnoye SDO–created engines, propulsions systems for ballistic missiles and space rockets that are unique by their characteristics and scope of functions, the engines, propulsions systems for spacecraft, LV upper stages and transfer orbit stages can be developed in short terms and at minimal costs.

Key words: liquid rocket engine, developed engines, testing, Yuzhnoye SDO, accumulated experience

Bibliography:
1. Liquid Rocket Engines, Propulsion Systems, Onboard Power Sources Developed by Propulsion Systems Design Office of Yuzhnoye SDO / Under scientific editorship of S. N. Konyukhov, Academician of NAS of Ukraine, V. N. Shnyakin, Candidate of Engineering Science. Dnepropetrovsk, 2008. 466 p.
2. Shnyakin V. N., Shulga V. A., Dibrivny A. V. Possibilities of Creating New LRE Based on Mature Technologies. Space Technology. Missile Armaments: Collection of scientific-technical articles. 2011. Issue 2. P. 61-71.

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