Search Results for “enterprise” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Thu, 25 Apr 2024 06:51:09 +0000 en-GB hourly 1 https://wordpress.org/?v=6.2.2 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “enterprise” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 13.1.2017 Reliability Evaluation of ILV Thermostating System Mating Hoses https://journal.yuzhnoye.com/content_2017_1/annot_13_1_2017-en/ Fri, 22 Sep 2023 15:13:28 +0000 https://journal.yuzhnoye.com/?page_id=29483
2 Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine 1 ; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine 2 Page: Kosm.
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13. Reliability Evaluation of ILV Thermostating System Mating Hoses

Authors:

Bigun S. O.1, Khorolskyi M. S.2, Skokov O. I.2

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine1; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine2

Page: Kosm. teh. Raket. vooruž. 2017 (1); 84-87

Language: Russian

Annotation: The technique is proposed of reliability evaluation of space launch vehicle low pressure air thermostating system joints hoses. By calculation method, high reliability level was confirmed of hoses of joints being an interface elements of launch vehicle launch complexes.

Key words:

Bibliography:
1. Development of Single Action Units’ Hoses of Cyclone-4 Space Launch System Thermostating System: SOW for R&D 2G40.12.8599.608TЗ/Yuzhnoye SDO. 2009. 41 p.
2. Abramov E. I., Kolesnichenko K. A., Maslov V. T. Hydraulic Actuator Elements (Guide). Kyiv, 1969. 320 p.
3. Shor Y. B., Kuzmin F. I. Tables for Reliability Analysis and Control. М, 1968. 286 p.
4. Ventsel E. S. Theory of Probability. М., 1964. 576 p.

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13.1.2017 Reliability Evaluation of ILV Thermostating System Mating Hoses
]]> 15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points https://journal.yuzhnoye.com/content_2018_2-en/annot_15_2_2018-en/ Thu, 07 Sep 2023 12:09:41 +0000 https://journal.yuzhnoye.com/?page_id=30786
2 Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine 1 ; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine 2 Page: Kosm.
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15. Topical Issues of Creation of Space Rocket Thermostatic System Mating Points

Authors:

Bigun S. O.1, Khorolskyi M. S.2

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine1; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine2

Page: Kosm. teh. Raket. vooruž. 2018 (2); 132-138

DOI: https://doi.org/10.33136/stma2018.02.132

Language: Russian

Annotation: The problem is defined of designing the space rocket low-pressure air thermostating systems joints. The basic requirements imposed to the joints from the side of space rocket and ground complex are determined and stated. For this purpose, the analysis of operating conditions and possible situations during rocket launches is made. Besides, the methodological principles based on problematic, systematic, and structuralfunctional approach were applied using the theoretical and empirical capabilities, attraction of general scientific and special investigation methods, as well as historical and logical methods. The list of topical issues is reflected for implementation in joint’s design. The ways are proposed to create the joints meeting the requirements imposed. As a result, it was ascertained that the joints can be made of simpler and at the same time failure-free design in the form of combined triune rubber hose fitted with a metal fixation/release unit installed on a sealing flange in a special groove. Of special note is the versatility of the proposed technical solution for use in any of the space launch systems known in the world’s practice. The article is concluded with following: the basic requirements have been formulated for ground complexes thermostating systems joints to ensure space rockets prelaunch processing and launch, in doing so, the topical problems were defined; the scientific principles were proposed to design the thermostating systems joints for comprehensive solution of the topical problems , including potential critical situations; the thermostating systems joints have been developed, manufactured and have successfully passed the ground development tests with simulation of the conditions maximally close to operating ones at static operating air pressures and in off-nominal situations.

Key words: planetary roving vehicle, self-propelled modular platform, generic module, interchangeability

Bibliography:
1. Bigun S. A., Khorolsky M. S et al. Types and Design Features of Thermostating System Mating Points of Launch Vehicle Payload Units and Launch Vehicle and Spacecraft Bays. Space Technology. Missile Armaments: Collection of scientific-technical articles. 2013. Issue 1. 123 p.
2. Bigun S. A., Khorolsky M. S et al. Experimental Investigations of Cyclone-4 ILV Thermostating System Mating Points Test Results. Space Technology. Missile Armaments: Collection of scientific-technical articles. 2016. Issue 2. 105 p.

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(Series “Normative Base of Enterprise”). Method of Automated Monitoring of the State of Enterprise’s Normative Documentation Collection.
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15. The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice

Authors:

Shipko O. F., Matus G. V., Il’ina S. M., Fesenko E. Y.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2018 (1); 91-100

DOI: https://doi.org/10.33136/stma2018.01.091

Language: Russian

Annotation: The article presents the main results obtained when solving the standardization tasks in Yuzhnoye SDO practice. The specific ways are presented of reducing the periods of work performance and increasing the accuracy of results due to the use of automated methods. The article also presents the recommendations in respect of sequence and methods of creating the standard data arrays, which allows optimizing the work process performance.

Key words:

Bibliography:
1. Matus G. V., Rud’ko K. V. Normalization of Terms of International Standards in Space Sphere. Standardization, Certification, Quality. 2013. No. 5. P. 19-24.
2. Shipko O. F., Matus G. V. Results of Using the Procedure of Terminological Monitoring for the Purpose of Normalization of Terms of International Standards in Space Sphere. Standardization, Certification, Quality. 2016. No. 3. P. 23-28.
3. ISO 10795:2011. Space Systems: Programme Management and Quality: Vocabulary. First edition 2011-08-15. Published in Switzerland: ISO, 2011. 37 p.
4. Classifier of Professions: DK 003:2010. (Effective from 2010-11-01). K., 2010. 746 p. (National Classifier of Ukraine).
5. Unified System of Design Documentation. Basic Provisions: Guide in Ukrainian and Russian / Under the general editorship of V. L. Ivanov. Lviv, 2001. 272 p. (Series “Normative Base of Enterprise”).
6. Streltsov E. V., Kolesnik N. Y. Method of Automated Monitoring of the State of Enterprise’s Normative Documentation Collection. Space Technology. Missile Armaments: Collection of scientific-technical articles / Yuzhnoye SDO. Dnepropetrovsk, 2015. No. 3. P. 99-102.
7. Fesenko E. Y., Kremena E. V. Design Documentation: Method of Automated Monitoring of Normative Documents Designations. Standardization, Certification, Quality. 2016. No. 2. P. 29-31.
8. The Law of Ukraine “On Standardization” dated 05.06.2014 No 1315-VII / News of Supreme Rada of Ukraine. 2014. No. 31. 1058 p. (With changes introduced as per Laws dated 15.01.2015 No. 124-VIII / News of Supreme Rada of Ukraine. 2015. No. 14. 96 p.).
9. Ukrainian Classifier of Normative Documents (ICS:2005, MOD): DK 004:2008. (Effective from 2009-04-01). К.: (Derzhspozhivstandard) State Consumption Standard of Ukraine, 2009. 97 p. (National Classifier of Ukraine).
10. Classification of Economic Activity Types: DK 009:2010. (Effective from 2012-01-01). К.: (Derzhspozhivstandard) State Consumption Standard of Ukraine, 2010. 42 p. (National Classifier of Ukraine).
11. State Classifier of Products and Services: DK 016:2010: [in 8 books]. (Effective from 2012-01-01). К.: (Derzhspozhivstandard) State Consumption Standard of Ukraine, 2010. (National Classifier of Ukraine). Book 1. 2011. 200 p. Book 2. 2011. 194 p. Book 3. 2011. 343 p. Book 4. 2011. 359 p. Book 5. 2011. 317 p. Book 6. 2011. 345 p. Book 7. 2011. 262 p. Book 8. 2011. 291 p.
12. Shipko A. F., Matus G. V. Methods to Improve Standardization Activity in Space Sphere. Space Technology. Missile Armaments: Collection of scientific-technical articles / Yuzhnoye SDO. Dnepropetrovsk, 2015. No. 3. P. 92-98.

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15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice
]]> 13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses https://journal.yuzhnoye.com/content_2018_1-en/annot_13_1_2018-en/ Tue, 05 Sep 2023 06:52:56 +0000 https://journal.yuzhnoye.com/?page_id=30469
2 Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine 1 ; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine 2 Page: Kosm.
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13. On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses

Authors:

Bigun S. O.1, Yevchik V. S.2, Khorolskyi M. S.2

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine1; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine2

Page: Kosm. teh. Raket. vooruž. 2018 (1); 72-84

DOI: https://doi.org/10.33136/stma2018.01.072

Language: Russian

Annotation: A series of materials is proposed for creation of space launch vehicle low-pressure air thermostating systems joints hoses. The topical issues are considered of materials designing with consideration for specific features of the hoses as special industrial rubber articles of launch vehicle launch sites.

Key words:

Bibliography:
1. Raw Stuff and Materials: Inf. Bull. М., 1999. No. 1. 44 p. https://doi.org/10.1007/978-1-4615-2802-9_3
2. Svitlichna R. F., Lotakov V. S., Chumicheva N. P. State and Prospects of Using Rubbers of New Generation in Rubber Industry of Ukraine: Scientific-Technical Report. К., 2001. No. 3. 13 p.
3. Nesterova L. A., Reznichenko S. V., Noskova L. F. et al. Experience of Using BNKS Paraffinate Nitrile Rubber in Formulations of Oil-Resistant Rubbers of Various Purpose at JSC “Uralsky Zavod RTI”. Med. Conf. on rubber: Collection of abstracts. М., 2000. No. 4. 121 p.
4. Investigation to Select Optimal Options of Replacing Raw Materials and Rubbers with Specifying Guaranteed Service and Storage Life of Rubber Products Being Components of Special Articles: Scientific–Technical Report DO-473-2002 UNUKTI DINTEM SE. 2002. 47 p.
5. Raw Stuff and Materials: Inf. Bull. М., 1999. No. 5. 55 p.
6. Raw Stuff and Materials: Inf. Bull. М., 2001. No. 3. 90 p.
7. Raw Stuff and Materials: Inf. Bull. М., 2001. No. 3. 96 p.
8. Raw Stuff and Materials: Inf. Bull. М., 2000. No. 3. 43 p.
9. Lotakov V. S., Yevchik V. S., Utlenko E. V. et al. Investigation of Operability of Rubbers with Adhesion Additives in Rubber-Metal Valves. Manufacture of Tires, Rubber Products and ATI. М., 1980. No. 4. P. 43-44.
10. Lotakov V. S., Yevchik V. S., Markova L. A. et al. Investigation of Alkali Impact on Adhesive Properties of Ethylene-Propylene Vulcanizing Agents. Caoutchouc and Rubber: Scientific–Technical Report. UNIKTI-DINTEM SE. 1981. No. 6. P. 18-19.
11. Svitlichna R. F., Bogutska E. O., Lotaakov V. S. et al. Technical Carbon of N Series. Prospects of Using in Rubber Mixtures of Caoutchoucs of New Generation: Scientific–Technical Report. К., 2006. No. 3. P. 17-20.
12. Yevchik V. S., Bogutskaya E. A., Khorolsky M. S. Investigations to Select Optimal Options of Replacing Raw Materials and Rubbers with Specifying Guaranteed Service and Storage Life of Rubber Products Being Components of 11K77 Article: Scientific–Technical Report DO-468-2000, UNIKTI-DINTEM SE. 2000. 55 p.
13. Nudelman Z. N., Lavrova L. N. Effective Vulcanization of Fluorine Rubbers. The III Ukr. International Scientific-Technical Conference of Rubber Industry Workers: Collection of abstracts. Dnepropetrovsk, 2000. 43 p.
14. Semyonov G. D., Yevchik V. S., Zaitseva T. P., Lotakov V. S. Prospects of Using New Vulcanizing Systems in Rubber Mixtures Based on Fluoroelastomers: Scientific–Technical Report. К., 2001. No. 3. 18 p.
15. Yevchik V. S., Zaitseva T. P., Khorolsky M. S. Investigations of Physical-Mechanical Characteristics of Rubbers Based on Caoutchoucs of New Generation: Scientific–Technical Report DO-387-89, DF VNIIEMI. Dnepropetrovsk, 2000. 61 p.
16. Belozerov N. V. Rubber Technology. М., 1979. 201 p.
17. Blokh G. A. Organic Rubber Vulcanization Accelerators. М.,1964. 156 p.
18. Big Reference Book of Rubber Industry Worker in 2 parts. Part 1. Rubbers and Ingredients / Under the general editorship of S. V. Reznichenko and Y. L. Morozov. М., 2012. 740 p.
19. Polyurethane Chemistry and Technology: Collection of conference papers. Manchester, 1967. 254 p.
20. Degteva T. G. et al. The Impact of Additives on Thermal Ageing of Rubbers and Model Gaskets Made of SKEP. Caoutchouc and Rubber. М., 1984. No. 8. P. 17-19.
21. Lepetov V. A. Rubber Products. L., 1976. 440 p.
22. Lepetov V. A., Yurtsev L. N. Calculations and Designing of Rubber Products and Production Accessories. М., 2009. 417 p.
23. New Prospective Hoses and Scarce and Commercially Inviable Rubbers, Ingredients and Materials: Recommendation No. 51-РМ-22/38/57/50-1050-83. М., 1983. 42 p.
24. Kornev A. E. et al. Technology of Elastomer Materials. М., 2009. 504 p.
25. Gerasimenko A. А. Protection of Machines from Biological Damages. M., 1984. 92 p.
26. Principles of Constructing Formulations and Using Rubbers for Rubber Products of Tropical Version: Recommendation No. 51-РМ-26-48-66. М., 1966. 56 p.
27. Assessment of Rubber Resistance to Damage by Thermites: Recommendation No. 51-РМ-4-622-75. М., 1975. 36 p.
28. Increasing Rubber Products Service Life in Conditions of Tropical Climate: Recommendation No. 51-РМ-4-697-76. М., 1976. 23 p.
29. Assessment of Rubber Resistance to Mould: Recommendation No. 51-РМ-4-407-73. М., 1976. 42 p.

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13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses
13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses
13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses
]]> 13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance https://journal.yuzhnoye.com/content_2016_2-en/annot_13_2_2016-en/ Tue, 06 Jun 2023 12:01:44 +0000 https://journal.yuzhnoye.com/?page_id=28327
2016 (2); 80-84 Language: Russian Annotation: The paper describes development of the devices for the nuclear quadrupole resonance thermometry at Yuzhnoye SDO and other Ukraine’s enterprises and considers capabilities of the enterprises to manufacture such devices.
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13. Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance

Authors:

Karpenko V. D., Solod S. D., Kolesnichenko V. K., Pokatayev V. M., Suvorov O. G.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2016 (2); 80-84

Language: Russian

Annotation: The paper describes development of the devices for the nuclear quadrupole resonance thermometry at Yuzhnoye SDO and other Ukraine’s enterprises and considers capabilities of the enterprises to manufacture such devices. Also given is refined analytical dependence for temperature calculation using the frequency of the nuclear quadrupole resonance in Bertholette salt within the ±40°C temperature range.

Key words:

Bibliography:

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13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance
13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance
13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance
]]> 6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points https://journal.yuzhnoye.com/content_2016_2-en/annot_6_2_2016-en/ Tue, 06 Jun 2023 11:53:22 +0000 https://journal.yuzhnoye.com/?page_id=28312
2 Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine 1 ; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine 2 Page: Kosm.
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6. Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points

Authors:

Bigun S. O.1, Khorolskyi M. S.2, Skokov O. I.2, Kaplun S. V.2

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine1; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine2

Page: Kosm. teh. Raket. vooruž. 2016 (2); 43-51

Language: Russian

Annotation: The results of ground development test and investigation of Cyclone-4 ILV low-pressure air thermostating system joints are presented. The obtained test data is analyzed, and conclusions are drawn on the effect of different factors on joint performance including force action on ILV in disconnection. An assessment of applicability of the tested joints, as baseline design, on other similar space launch systems is performed.

Key words:

Bibliography:

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6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points
6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points
6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points
]]> 27.1.2019 Phases of Cooperation of Yuzhnoye SDO and Dnipro National University Physical Engineering Department on the Issues of Mutual Human Resourcing: Past, Present. Future https://journal.yuzhnoye.com/content_2019_1-en/annot_27_1_2019-en/ Wed, 24 May 2023 16:01:14 +0000 https://journal.yuzhnoye.com/?page_id=27732
2019, (1); 188-194 DOI: https://doi.org/10.33136/stma2019.01.189 Language: Russian Annotation: This paper in brief presents the history of cooperation between the Yuzhnoye State Design Office (YSDO) and University’s applied-physics faculty focused on drawing the enterprise specialists to teaching activity at the faculty, and University graduates – to work at the enterprise. Key words: cooperation , enterprise , faculty , staff , experts , graduates , students , applicants Bibliography: 1. cooperation , enterprise , faculty , staff , experts , graduates , students , applicants .
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27. Phases of Cooperation of Yuzhnoye SDO and Dnipro National University Physical Engineering Department on the Issues of Mutual Human Resourcing: Past, Present. Future

Authors:

Linnik A. K.

Organization:

Oles Honchar Dnipro National University, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2019, (1); 188-194

DOI: https://doi.org/10.33136/stma2019.01.189

Language: Russian

Annotation: This paper in brief presents the history of cooperation between the Yuzhnoye State Design Office (YSDO) and University’s applied-physics faculty focused on drawing the enterprise specialists to teaching activity at the faculty, and University graduates – to work at the enterprise. Interchange of personnel throughout three periods is analyzed: a) in the remote past (early 1950s – late 1980s); b) watershed years at the turn of millennia (early 1990s – mid 2010s) and c) nowadays (from mid 2010s). Forecast attempt for the near future is also made. Active participation of the outstanding YSDO specialists in the organization and education at the faculty, especially at the first stage of cooperation, is shown. In particular, Y. A. Smetanin, YSDO Deputy General Designer, was the head of department №1, N. S. Shnyakin was the head of department №2, department №3 was chaired by N. F. Gerasyuta – Head of Dynamics, Ballistics and Control Department in YSDO. At that period faculty trained annually all in all ~300 young specialists for Yuzhnoye State Design Office. Great deal of problems and new challenges, which emerged in watershed 1990s, are described. Despite this, close cooperation between the YSDO and faculty was basically maintained. Thus, for example, for several years S. N. Konyukhov, YSDO General Designer, chaired the state examination board on defence of graduation works of the department №1 students. At the same time, number of aerospace specialties graduates this period has sharply decreased to 35 graduates. The present state of affairs, causing concern, is shown. Actual admission rate for the aerospace specialties for the past years suggests that starting with 2022, number of graduates for Yuzhnoye State Design Office can practically reduce to nothing.

Key words: cooperation, enterprise, faculty, staff, experts, graduates, students, applicants

Bibliography:
1. Sekretniy pidrozdil galuzi: Narysy istorii physiko-technochnogo institute Dnipropetrovskogo natsionalnogo universitetu; M. V. Polyakov (kerivnik redkol). D.: Bid-vo Dnipropetr. un-tu. 2001. 376 p.
2. Kafedra kosmicheskikh informatsionnykh technologiy/ www.fti.dnu.
3. Strategichniy plan rozvytku DP KB “Pivdenne” na 2017-2021.

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27.1.2019 Phases of Cooperation of Yuzhnoye SDO and Dnipro National University Physical Engineering Department on the Issues of Mutual Human Resourcing: Past, Present. Future
27.1.2019 Phases of Cooperation of Yuzhnoye SDO and Dnipro National University Physical Engineering Department on the Issues of Mutual Human Resourcing: Past, Present. Future
27.1.2019 Phases of Cooperation of Yuzhnoye SDO and Dnipro National University Physical Engineering Department on the Issues of Mutual Human Resourcing: Past, Present. Future

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2 Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine 1 ; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine 2 Page: Kosm.
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11. Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses

Authors:

Bigun S. O.1, Khorolskyi M. S.2

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine1; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine2

Page: Kosm. teh. Raket. vooruž. 2019, (1); 76-80

DOI: https://doi.org/10.33136/stma2019.01.076

Language: Russian

Annotation: The range of problems of development testing of thermostating systems mating hoses for the needs of space rocketry building is most topical. In publications, insufficient attention is given to the presented range of problems. The purpose of this article is to fill in this gap. Testing of the hoses performed in accordance with comprehensive program implies a number of sequential tests and has its peculiarities. Generally, these are factory tests, participation in system and integrated tests and participation in flight tests of a space rocket. Special reference was made to the role of accelerated climatic tests, as a part of factory tests, to confirm warranty obligations for the hoses. In conclusion of the article, the concept was formulated on organization of development testing of space rockets thermostating systems hoses that reflects test peculiarities and the conclusion was made that conducting the testing of hoses according to the presented sequence ensures creation of articles that meet the requirements imposed.

Key words: space launch system, launch site, launch complex, comprehensive development test program, test program and procedure, accelerated climatic tests, integrated tests

Bibliography:

1. Degtyarev A. V., Kashanov A. E., Krivobokov L. V. Systemnyi podkhod k planirovaniyu eksperimentalnoy otrabotki novykh i modernizuemykh raket-nositeley /Systemnye technologii: Regional. mezhvuz. sb. nauch. trudov. 2011. 196 p.
2. Dunaev D. V., Krivobokov L. V. Obosnovanie vidov ispytaniy pri sozdaniy compleksnoi programmy eksperimentalnoy otrabotki typovoy rakety kosmicheskogo naznacheniya/ Aviatsionno-kosmicheskaya technika I technologia. №4. 2015. P. 26-31.
3. Dunaev D. V., Krivobokov L. V. Analiz matematicheskikh modeley otsenki nadezhnosti raketnoy techniki pri eksperimentalnoy otrabotke/ Kosmicheskaya technika. Raketnoe vooruzhenie: Sb. nauch.- techn. st. 2015. Vyp. 1. Dnepropetrovsk: GP KB «Yuzhnoye». P. 3-8.
4. Bigun S. O., Chorolskiy M. S. Shlyakhi stvorennya vuzliv stykuvannya system termostatuvannya raket kosmichnogo pryznachennya/ Cholodilna technika I technologia: Nauk.-techn. journal. 2018. T. 54. Vyp. 1. Odessa: ONAKhT. P. 27-30.
5. Bigun S. A., Skokov A. I. Razrabotka I sozdanie ustanovki dkya ispytaniy uzlov stykovki system termostatirovaniya raket-nositeley/ Kosmicheskaya technika. Raketnoye vooruzhenie: Sb. nauch.- techn. st. 2015. Vyp. 3. Dnepropetrovsk: GP KB «Yuzhnoye». P. 107-110.
6. Bigun S. A., Khorolskiy M. S. i dr. Eksperimentalnyie issledovania rezultatov otrabotrki uzlov stykovki systemy termostatirovania RKN Cyclone-4 / Kosmicheskaya technika. Raketnoye vooruzhenie: Sb. nauch.- techn. st. 2016. Vyp. 2. Dnepropetrovsk: GP KB «Yuzhnoye». P. 43-51.
7. KRK Cuclone-4. Rukava uzlov razovogo deistviya systemy termostatirovania 2G40 i rukava stykovki adaptera transportnoy systemy termostatirovania 2G20: Complexsnaya programma eksperimentalnoy otrabotki D4301.25009. 00.00 KPEO/GP UNIKTI DINTEM, GP KB «Yuzhnoye». 2011. 20 p.

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11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses
11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses
11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses

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1 Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine 1 ; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine 2 Page: Kosm.
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7. Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems

Authors:

Khorolskyi M. S.2, Bigun S. O.1

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine1; State Enterprise “Ukrainian Research Design-Technological Institute of Elastomer Materials and Products”, Dnipro, Ukraine2

Page: Kosm. teh. Raket. vooruž. 2023 (1); 63-69

DOI: https://doi.org/10.33136/stma2023.01.063

Language: Ukrainian

Annotation: Explosive bolts are widely used as actuating devices in the spacecraft separation systems. Explosive bolt body is divided into parts as a result of engagement of the pyromixture placed inside. Activated explosive bolts have negative mechanical effect on the interface elements and sensitive electronic devices installed nearby owing to explosive behavior of the pyromixture combustion, generating shock front with high pressure and velocities, impacts and collisions of the structural units. Cumulative effect of the above factors on the separated objects is called pyroshock. For separation systems with increased requirements to external actions and cleanliness, authors developed a shear explosive bolt or pyrobolt, divided into parts, cutting the body walls in segments, which are set in motion by action of the pressure of gases, released as a result of pyrocartridge activation. The basic sources of pyroshock for these shear explosive bolts with segments are: combustion of pyromixture, internal impacts of structural units against the bolt body; cutting of body wall in segments, release of preliminary deformed interface after activation. Structural solutions are presented to reduce the pyroshock per each of the components. Vibration impulsive loading during pyromixture combustion is reduced by optimization of explosive quantity, finding its minimum to provide the reliable activation of the device. To reduce the impact on the explosive bolt elements and shock front interface the rubber gasket is installed in the path of shock wave distribution, partially disseminating and absorbing its kinetic energy. Damper, made of easily deformable aluminum alloy, is also installed to decrease the internal impact of the rod against the explosive bolt body. Functional testing of the device, using the pendulum suspension and measuring separation speed and vibration impulsive loading, showed that body parts of the shear explosive bolt with segments are separated without significant impact loads and discharge of high-temperature gases and debris, providing reliable separation of compartments and units without damaging the sensitive equipment. Obtained values of the mechanical momentum, I = 0,4÷0,7 N•s and shock load spectrum – g-load 1950 g at the frequency range up to 5000 Hz, meet the up-to-date requirements to pyrotechnical devices.

Key words: explosive bolt, pyroshock, shock wave, pyrocartridge, high-temperature gases, damper

Bibliography:
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2. Bigun S. A., Khorolskiy M. S. Problemnye voprosy sozdania uzlov stykovki system termostatirovania raket kosmicheskogo naznachenia. Kosmicheskaya technika. Raketnoe vooruzhenie. Space technology Missile armaments: sb. nauch.-techn. st. GP «KB «Yuzhnoye». Dnepropetrovsk, 2013. Vyp. 2. S. 132-138.
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10. Bigun S. A., Yevchik V. S., Khorolskiy M. S. O vybore materialov dlya sozdaniya rukavov stykovki system termostatirovania sovremennyh RKN. Kosmicheskaya technika. Raketnoe vooruzhenie. Space technology Missile armaments: sb. nauch.-techn. st. GP «KB «Yuzhnoye». Dnepr, 2018. Vyp. 1. S. 72-84. https://doi.org/10.33136/stma2018.01.072
11. Pat. Ukrainy № 120445, 2019 r., В64G 5/00, В64G 1/40, F16L 37/08, F41F 3/055, F16L 33/00.
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13. Khorolskiy M. S., Bigun S. O. Shodo kontseptsii stvorennya vuzliv stykuvannya system termostatuvannya raket kosmichnogo pryznachennya. Systemne proektuvannya i analiz characteristic aerokosmichnoi techniki: zb. nauk. pr. 2019. T. XXVII. S. 162-168.
14. Bigun S. A., Khorolskiy M. S. i dr. Eksperimentalnye issledovania rezultatov otrabotki uzlov stykovki system termostatirovania RKN «Tsiklon-4». Kosmicheskaya technika. Raketnoe vooruzhenie: sb. nauch.-techn. st./ GP «KB «Yuzhnoye». Dnepropetrovsk, 2016. Vyp. 2. S. 43-51.

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7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems
7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems
7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems

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]]> 3.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development https://journal.yuzhnoye.com/content_2023_1-en/annot_3_1_2023-en/ Fri, 12 May 2023 16:10:31 +0000 https://test8.yuzhnoye.com/?page_id=26987
Authors observed the importance of reconstruction and upgrading of multiple launch rocket systems of Grad 9К51, Hurricane 9К57 and Tornado 9К58 types and missiles they use by the enterprises of the domestic military-industrial complex. The article dwells on the main areas of upgrading of the multiple launch rocket system Grad 9K51 performed by NPO Splav and co-operating enterprises in 1997‒1998 for a foreign customer.
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3. Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development

Authors:

Aksenenko O. V., Hurskyi O. I., Klochkov A. S., Kondratiuk Ye. A., Shyniberov D. O.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2023 (1); 31-40

DOI: https://doi.org/10.33136/stma2023.01.031

Language: Ukrainian

Annotation: The article dwells on the multiple launch rocket systems with high firepower, firing rate and manoeuvrability, which continue to be one of the basic means of destruction of the land forces in the conditions of the modern armed conflicts. Authors observed the importance of reconstruction and upgrading of multiple launch rocket systems of Grad 9К51, Hurricane 9К57 and Tornado 9К58 types and missiles they use by the enterprises of the domestic military-industrial complex. The article dwells on the main areas of upgrading of the multiple launch rocket system Grad 9K51 performed by NPO Splav and co-operating enterprises in 1997‒1998 for a foreign customer. The key factors that allowed improving the performance of the Grad system in the upgrading process are identified in this article. The main characteristics of the unguided missiles 9M217, 9M218, 9M521, 9M522, designed for the foreign customer, had been investigated. The performance characteristics of the Tornado-G multiple launch rocket system which went into service with the Ministry of Defense of the Russian Federation in 2014, as well as the family of the upgraded unguided missiles 9M538, 9M539, 9M641, are analyzed. The article identifies the main areas of work for further improvement of the performance characteristics of the 122-mm unguided missile, developed by Yuzhnoe Design Office for the multiple launch rocket system 9K51 Grad. This article can be useful for the specialists in development of new and upgrading outdated systems of rocket weapons.

Key words: multiple launch rocket system (MLRS), missile, 9K51 Grad, 9M217, 9M218, 9M521, 9M522, Tornado-G, 9M538, 9M539, 9M541

Bibliography:
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3. Kapustnik-B. Kompleks sredstv avtomatizirovannogo upravleniya ogniem (indeks 1В126). URL: http://roe.ru/catalog/sukhoputnye-vosyka/kompleksy-sredstv-avtomatizirovannogo-upravleniya-ognem-artillerii/kapustnik-b/
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14. 9M521.122-mm neupravlyaemiy oskolochno-fugasniy reaktivniy snaryad s golovnoi chastiu povyshennogo moguschestva. URL: http://roe.ru/catalog/sukhoputnye-vosyka/boepripasy/9m521/
15. 9M522. 122-mm neupravlyaemiy oskolochno-fugasniy reaktivniy snaryad s otdelyaemoy oskolochno-fugasnoy golovnoi chastiu (indeks 9М522). URL: http://roe.ru/catalog/sukhoputnye-vosyka/boepripasy/9m522/
16. 9M217. 122-mm neupravlyaemiy reaktivniy snaryad s samopritselivayuschimisya boevymi elementami (indeks 9М217). URL: http://roe.ru/catalog/sukhoputnye-vosyka/boepripasy/9m217/
17. 9M218. 122-mm neupravlyaemiy reaktivniy snaryad s kumulyativno-oskolochnymi boevymi elementami (indeks 9M218). URL: http://roe.ru/catalog/sukhoputnye-vosyka/boepripasy/9m218/
18. TRG-122 Guided Rocket – Roketsan. URL: www.roketsan.com.tr/en/product/trg-122-guided-rocket/
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21. Reaktivniy snaryad 9M218 s kassetnoy GCh. URL: http://rbase.new-factoria.ru/missile/wobb/grad/9m218.htm
22. PAO «Motovilihinskie zavody» vypolnilo goskontrakt po RSZO “Tornado-G”. URL: https://topwar.ru/164625-pao-motovilihinskie-zavody-vypolnilo-goskontrakt-po-rszo-tornado-g.html
23. Neupravlyaemiy reaktivniy snaryad 9M538. URL: http://rbase.new-factoria.ru/missile/wobb/8779/8779.shtml
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26. 122-mm reaktivnye snaryady dlya RSZO “Tornado-G”. URL: https://bmpd.livejournal.com/3326341.html

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3.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development
3.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development
3.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development

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