Search Results for “Pustovharov A. A.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Tue, 10 Mar 2026 09:53:19 +0000 en-GB hourly 1 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “Pustovharov A. A.” – 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. ORCID authors: Pustovharov A. 6 Singapore Singapore; Singapore; Singapore; Singapore; Singapore; Singapore 6 Ukraine Kyiv; Odessa; Dnipro; Kremenchuk 4 France Paris; Paris; Paris 3 Germany Limburg an der Lahn; Falkenstein 2 Vietnam 1 Brazil 1 Kuwait Kuwait City 1 Albania Tirana 1 Iran Tehran 1 Poland Poznan 1 India Delhi 1 Downloads, views for all articles Articles, downloads, views by all authors Articles for all companies Geography of downloads articles Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A.
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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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]]> 6.2.2025 Floating launch platform of a sea-based space launch site https://journal.yuzhnoye.com/content_2025_2-en/annot_6_2_2025-en/ Tue, 27 Jan 2026 08:37:10 +0000 https://journal.yuzhnoye.com/?page_id=35831
Floating launch platform of a sea-based space launch site Date of receipt of the article for publication: 07.12.2025 Date of acceptance of the article for publication after review: 22.12.2025 Date of publication: 27.01.2026 ISSN: 2617-5525 e-ISSN: 2617-5533 Authors: Pustovharov A. ORCID authors: Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A. Pustovharov A.
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6. Floating launch platform of a sea-based space launch site

Date of receipt of the article for publication: 07.12.2025

Date of acceptance of the article for publication after review: 22.12.2025

Date of publication: 27.01.2026

ISSN: 2617-5525

e-ISSN: 2617-5533

Authors:

Pustovharov A. A.

ORCID authors:

Pustovharov A. A. ORCID

Organization:

Yangel Yuzhnoye State Design Office

Page: Kosm. teh. Raket. vooruž. 2025 (2); 58-66

DOI: https://doi.org/10.33136/stma2025.02.058

Language: Ukrainian

Annotation: One of the courses in the evolution of space rocket complexes is the relocation of launch sites for space launchers to the World Ocean. Firstly, it provides the opportunity to render space services for countries that encounter complications in fi nding locations for spaceports on land. Secondly, it allows for a larger number of launch azimuths. Thirdly, it helps to increase the payload capabilities of space launchers lifting from launch sites closer to the equator. The article reviews the current global progress in utilizing ships as part of sea-based space launch sites. It notes that more and more countries are becoming interested in the development and construction of maritime space launch sites. As one of the leading enterprises in the rocket and space industry, Yuzhnoye State Design Offi ce also conducts relevant research and development, which has already yielded a conceptual design for such a launch site for the Cyclone-1K lightweight space launcher. A specifi cally equipped naval vessel was selected as the launch platform for this rocket. The article outlines initial data applied for the overall design of the launch facility and the launch platform in particular. The design process involved modern software for 3D modeling and fi nite element analysis. A conceptual view and the primary characteristics of the launch platform, obtained through the design, are presented. The platform’s primary systems are described. The specifi city of equipment arrangement to support launch vehicle preparation and ensure the liftoff , as well as the relation between such arrangement and the launch platform’s appearance and internal structure, are demonstrated. The results of this work will be valuable for the practical implementation of the sea-based space launch site project. A fl oating launch platform is the essential element of a sea-based space launch facility, as it accommodates everything necessary for launching space rockets from the sea surface. Thanks to the versatility of the fl oating launch platform, it is possible to outline its appearance and characteristics according to the strategy for the launch services market.

Key words: sea launch, sea-based space launch site, space launcher, fl oating launch platform

Bibliography:

1. Jeff Foust, February 14, 2023. SpaceX drops plans to convert oil rigs into launch platforms. URL: https://spacenews.com/ spacex-drops-plans-to-covert-oil-rigs-into-launch-platforms (data zvernennia 25.09.2025).
2. A Spaceport for Germany. The driver for a strong business and aerospace location. URL: https://www.offshore-spaceport.de/en (data zvernennia 25.09.2025).
3. Andrew Jones, December 9, 2022. China launches 14 satellites with new solid rocket from mobile sea platform. URL: https://spacenews.com/china-launches-14-satellites-with-new-solid-rocket-from-mobile-sea-platform (data zvernennia 25.09.2025).
4. Andrew Jones, January 13, 2025. Chinese sea launch sends 10 navigation enhancement satellites into orbit. URL: https://spacenews.com/chinese-sea-launch-sends-10-navigation-enhancement-satellites-into-orbit (data zvernennia 25.09.2025).
5. Andrew Jones, October 11, 2025. Huge commercial Chinese solid rocket launches 3 satellites from barge in the Yellow Sea. URL: https://spacenews.com/huge-commercial-chinese-solid-rocket-launches-3-satellites-from-barge-in-the-yellow-sea (data zvernennia 12.10.2025).
6. Larkin Yu. M., Onyshchenko A. F. Osoblyvosti proiektuvannia balkeriv. Visn. Odeskoho natsionalnoho morskoho universytetu. 2015. № 3 (45). S. 219 – 228.
7. Rehistr sudnoplavstva Ukrainy. Pravyla shchodo obladnannia morskykh suden. T. 2. Chastyny: ІІ «Korpus»; ІІІ «Prystroi, obladnannia i zabezpechennia»; ІV «Ostiinist»; V «Podil na vidsiky»; ХVІ «Konstruktsiia ta mitsnist korpusiv suden iz polimernykh kompozytsiinykh materialiv». Rehistr sudnoplavstva Ukrainy. 2020. 792 s.
8. Dontsov S. V. Osnovy teorii sudna. Odesa, 2020. 188 s.
9. Novikov A. I., Zinkovskii-Horbatenko V. H., Kot V. P. Vantazhna marka morskykh suden. Navch. posibn . Sevastopol, 2006. 160 s.
10. Hurs I. F. Praktychni rozrakhunki morekhidnykh yakostei sudna. Izmailskyi morskyi trenazhernyi tsentr. Izmail, 2001. 29 s.
11. Eyres D. J., Bruce G. J. Ship construction. 7th edition. Elsevier ltd, 2012. 388 p. https://doi.org/10.1016/B978-0-08-097239-8.00036-2
12. Syzov V. H. Teoriia korablia: Navch. posibn. Odeska nats. mor. akad. Odesa: FENIKS, 2003. 284 s.
13. Presentatsiia rushiiv Azipod® serii VI. Buklet firmy ABB Oy, Marine. 2010. 36 s.
14. WST-24R Retractable Thruster. Buklet firmy Wärtsilä Corporation. 2017. 2 s.

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]]> 5.1.2025 Studying the landing of the reusable first stage of the Cyclone-5 space launch vehicle on a maritime landing platform https://journal.yuzhnoye.com/content_2025_1-en/annot_5_1_2025-en/ Wed, 27 Aug 2025 14:09:06 +0000 https://journal.yuzhnoye.com/?page_id=35485
, Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A. I., Pustovharov A.
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5. Studying the landing of the reusable first stage of the Cyclone-5 space launch vehicle on a maritime landing platform

ISSN: 2617-5525

e-ISSN: 2617-5533

Автори: Berdnyk O. I., Pustovharov A. A., Snehirov M. H.

Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2025 (1); 34-44

DOI: https://doi.org/10.33136/stma2025.01.034

Language: Ukrainian

Annotation: The development of reusable launch vehicles allowing for the recovery of their components (particularly the fi rst stages) is a logical step in the evolution of modern space rocket technology. Yuzhnoye State Design Offi ce, as one of the leading designers of space rocket technologies, engages in research eff orts concerning this issue. For example, a conceptual design of the Cyclone-5 space launch vehicle with a reusable fi rst stage was devised. A dynamic rocket landing using the primary propulsion system and specialpurpose legs was chosen as the recovery method for the fi rst stage. Considering the diffi culties in selecting landing areas for the fi rst stage, making it land on a seagoing platform in the sea seems reasonable. Such a platform may sail to the assigned location in advance and transport the fi rst stage after landing as close as possible to the space fl ight facility to prepare it for the next fl ight. This paper shows the potential designs of the fi rst stages of space launch vehicles and the seagoing landing platform. It also specifi es the parameters of such a platform and the ambient (environmental) factors to be considered when studying the landing of a space rocket’s fi rst stage. This paper also describes the study procedure and simulates some scenarios of the joint motion of the fi rst stage and the landing platform. The values and ratios of various parameters were determined from the analysis of the dynamics, and some relations were derived. The output of this work will be useful in proceeding to the practical realization of a space launch vechicle project with a reusable fi rst stage.

Key words: First stage recovery, environmental conditions at the landing location, parameters of seagoing platform motions, landing process simulation, the joint motion of a stage and a platform, the analysis of landing dynamics

Bibliography:

1. Atlas okeanov. Atlanticheskii i Indiiskii okeany. Glavnoie upravleniie navigatsii i okeanografii Ministerstva oborony Soiuza SSR. 1977. 306 s.

2. Ashyk V. V. Proiektirovaniie sudov: Uchebnik. 2-ie izd., pererab. i dop. L.: Sudostroieniie, 1985. 320 s., il.

3. Novikov A. I. Otsenka posadki, ostoichivosti i prochnosti sudna v protsesse ekspluatatsyi: uchebnoie posobiie. Sevastopol: Izd-vo SevNYU, 2003. 136 s., il. https://doi.org/10.2307/40158123

4. Borodai I. K., Netsveteiev Yu. A. Morekhodnost sudov. L.: Sudostroieniie, 1982. 288 s.

5. Semenov-Tian-Shanskii V. V., Blagoveshenskii S. N., Kholodilin A. N. Kachka koroblia. L.: Sudostroieniie, 1969. 392 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
Pustovharov А.
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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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]]> 9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software https://journal.yuzhnoye.com/content_2023_1-en/annot_9_1_2023-en/ Fri, 12 May 2023 16:11:14 +0000 https://test8.yuzhnoye.com/?page_id=26993
, Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O. I., Pustovharova O.
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9. Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software

ISSN: 2617-5525

e-ISSN: 2617-5533

Authors:

Yenotov V. H., Kushnir B. I., Pustovharova O. V., Chubarov A. M.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2023 (1); 77-87

DOI: https://doi.org/10.33136/stma2023.01.077

Language: Ukrainian

Annotation: Substantiation of the research tools has been performed as a part of methodology development for the air and missile defense system. The problem under consideration is very complex due to the multifactorial nature of the research object, its qualitative variety and manifold structure, incomplete definition of the problem statement. Furthermore, the ability of modern technologies to produce different arms systems, which are capable of carrying out same class tasks, considerably increases the risk of making not the best decisions. Based on this, as well as taking into account the sharp increase in the cost of weaponry, the considered problem is classified as an optimization one that should be solved through the theory of operations research. In this theory, such task is viewed as a mathematical problem, and mathematical simulation is the basic method of research. The main types of mathematical models, their areas of application have been considered as a part of the analysis. The classification of mathematical models has been indicated according to the scale of reproduced operations, purpose, and goal orientation. Quantitative and qualitative correlation of forces has been accepted as the efficiency criterion, which determines a goal orientation of the model. The problems related to this have been shown. In particular, searching for the compromise between simplicity of the mathematical model and its adequacy to the research object is among these problems. Two of the basic approaches to principles of the military operation model construction and its assessment have been considered. The first is implemented through modeling of the combat operations. The second approach is based on the assumption that different armament types can be compared based on their contribution to the outcome of the operation, and on the possibility to assign «a weighting coefficient» named as a combat potential to each of these types. The modern level of problem solving related to this method has been shown. The reasonability of its application in the considered task, including the definition of forces correlation of the opposing parties, has been substantiated. The basic regulations of the construction concept of the required mathematical model and tools for its research have been formulated based on the analysis results: the assigned problem should be solved by analytical methods through the theory of operations research; the analytical model is the most acceptable conception of the analyzed level of the military operation; the synthesis of the model should be based on the idea of a combat potential. At the same time, it should be taken into account that the known approach to the definition of forces correlation, which uses the combat potential method, has a number of essential limitations, including the methodological ones. Therefore, within the bounds of further research, this approach requires the development both in terms of improving the reliability of the single assessment and in terms of giving the system qualities to the synthesized mathematical model.

Key words: multifunctional system, mathematical model, military unit, combat potential, correlation of forces, defensive sufficiency

Bibliography:

1. Pavlyuk Yu. S. Ballisticheskoe proektirovanie raket: ucheb.-metod, posobie dlya vuzov. UDK623.451.8. Izd-vo ChGTU, Chelyabinsk, 1996. 92 s.
2. Nikolaev Yu. M., Solomonov Yu. S. Inzhenernoe proektirovanie upravlyaemykh ballisticheskikh raket s RDTT. M., 1979. 240 s.
3. Enotov V. G., Kirichenko A. S., Pustovgarova Ye. V. Osobennosti rascheta i vybora raskhodnoy diagrammy dvukhrezhimnykh marshevykh RDTT: ucheb.-metod. posobie. Pod red. akadem. A. V. Degtyreva. Dnepr, 2019. 68 s.
4. Enotov V. G., Kushnir B. I., Pustovgarova Ye. V. Metodika-programma proektnoy otsenki characteristic marshevykh dvigateley na tverdom toplive s korpusami iz vysokoprochnykh metallicheskikh materialov, statsionarnymi soplami i postanovka ee na avtomatizirovanniy raschet: ucheb.-metod. posobie. Vtoroe izd., pererabot. i dop. Pod red. A. S. Kirichenko. Dnep, 2019. 91 s.
5. Enotov V. G., Kirichenko A. S., Kushnir B. I., Pustovgarova Ye. V. Metodika proektnoy otsenki characteristic marshevykh dvigatelnykh ustanovok na tverdom toplive s povorotnymi upravlyayuschimi soplami, plastikovymi tselnomotannymi korpusamy i postanovka ee na avtomatizirovanniy raschet: ucheb.-metod. posobie. Vtoroe izd., pererabot. i dop. Pod red. akadem. A. V. Degtyareva. Dnepr. 2019. 149 s.
6. Alemasov V. Ye., Dregalin A. F., Tishin A. P. Teoriya raketnykh dvigateley. M., 1980. 55 s.
7. Raschetnye materialy dlya podgotovki i vydachi iskhodnykh dannykh na razrabotku uzlov marshevykh dvigatelnykh ustanovok na tverdom toplive. Raschet ID metodom avtomatizirovannogo proektirovaniya operativno-takticheskikh raket: inzhenern. zapiska 553-376 IZ. GP «KB «Yuzhnoye». Dnepropetrovsk, 2017. 30 s.
8. Metodika avtomatizirovannogo proektirovaniya operativno-takticheskikh raket: nauch.-tekhn. Otchet 03-453/32 NTO. GP «KB «Yuzhnoye». Dnepropetrovsk, 2010. 127 s.

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