Search Results for “space and aircraft technologies” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Tue, 03 Nov 2026 17:47:39 +0000 en-GB hourly 1 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “space and aircraft technologies” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 6.1.2026 An experimental and computational method for predicting the characteristics of dielectric products in the millimeter wave band https://journal.yuzhnoye.com/content_2026_1-en/annot_6_1_2026-en/ Tue, 03 Nov 2026 14:51:15 +0000 https://journal.yuzhnoye.com/?page_id=38047
Key words: rocket , space and aircraft technologies , dielectric materials , complex permittivity , millimeter wave band , free-space measurements , vector network analyzer , electromagnetic simulation Bibliography: 1. rocket , space and aircraft technologies , dielectric materials , complex permittivity , millimeter wave band , free-space measurements , vector network analyzer , electromagnetic simulation .
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6. An experimental and computational method for predicting the characteristics of dielectric products in the millimeter wave band

Date of receipt of the article for publication: 05.09.2026

Date of acceptance of the article for publication after review: 15.10.2026

Date of publication: 02.11.2026

ISSN: 2617-5525

e-ISSN: 2617-5533

Authors:

Khardikov V. V.1, Osinovyy H. H.2, Kozis K. V.2, Derevianko I. I.2, Kalynychenko D. S.2, Vinnichenko S. O.2

ORCID authors:

Khardikov V. V.1 ORCID, Osinovyy H. H.2 ORCID, Kozis K. V.2 ORCID, Derevianko I. I.2 ORCID, Kalynychenko D. S.2 ORCID, Vinnichenko S. O.2 ORCID

Organization:

Karazin Kharkiv National University, Kharkiv, Ukraine 1, Yuzhnoye State Design Office, Dnipro, Ukraine2

Page: Kosm. teh. Raket. vooruž. 2026, (1); 49-60

Language: Ukrainian

Annotation: The paper investigates an experimental and computational approach to the determination and prediction of the electrodynamic characteristics of dielectric products in the millimeter wave band. The relevance of the study is associated with the widespread use of dielectric materials in various radio engineering, telecommunication, measurement, and sensor systems, as well as with more and more demanding requirements for the accuracy in determining the electromagnetic parameters of these products at higher operating frequencies. Particular attention is paid to the determination of complex permittivity based on the results of free-space measurements using two antennas, followed by numerical data processing and electromagnetic simulation. The paper analyzes the specifi c features of the contact, coaxial, waveguide, resonant, and free-space methods for determining dielectric properties. It demonstrates that free-space techniques are advantageous for investigating complex-geometry fi nished products because they do not require the placement of the object inside a waveguide or a resonant structure and allow examination of relatively large-sized samples. The proposed approach involves measuring signal characteristics with a vector network analyzer, normalizing the results to the reference measurement, and accounting for the infl uence of antenna parameters, measurement system geometry, parasitic refl ections, transmission-path losses, and object placement accuracy. The paper discusses the feasibility of determining electromagnetic parameters by solving an inverse electromagnetic problem and conducting a numerical simulation. Combining experimental data with the geometric parameters of a product and its electromagnetic model enables the improvement of parameter estimation accuracy and the prediction of product characteristics over a specifi ed frequency range. Independent experimental verifi cation is considered a technique to assess the reliability of the results. The proposed approach can be practical for investigating dielectric materials and products for which the fabrication of specialized test specimens or the use of conventional waveguide and resonant measurement techniques is technically diffi cult or limited.

Key words: rocket, space and aircraft technologies, dielectric materials, complex permittivity, millimeter wave band, free-space measurements, vector network analyzer, electromagnetic simulation

Bibliography:

1. Liu X., Gan L., Yang B. Millimeter-wave free-space dielectric characterization. Measurement. 2021. Vol. 179. Art. 109472. https://doi.org/10.1016/j.measurement.2021.109472
2. Anferov A., Harvey S. P., Wan F., Lee K. H., Simon J. Schuster D. I. Low-loss millimeterwave resonators with an improved coupling structure. Superconductor Science and Technology. 2024. Vol. 37, Iss. 3. Art. 035013. https://doi.org/10.1088/1361-6668/ad22ff
3. Zwick T., Chandrasekhar A., Baks C. W., Pfeiff er U. R., Brebels S., Gaucher B. Determination of the complex permittivity of packaging materials at millimeter-wave frequencies. IEEE Transactions on Microwave Theory and Techniques. 2006. Vol. 54, Iss. 3. Р. 1001–1010. https://doi.org/10.1109/tmtt.2005.864140
4. Mirbeik-Sabzevari A., Tavassolian N.Characterization and Validation of the Slim-Form Open-Ended Coaxial Probe for the Dielectric Characterization of Biological Tissues at Millimeter-Wave Frequencies. IEEE Microwave and Wireless Components Letters. 2018. Vol. 28, Iss. 1. Р. 85–87. https://doi.org/10.1109/lmwc.2017.2772187
5. Dudeck K. E., Buckley L. J. Dielectric Material Measurement of Thin Samples at Millimeter Wavelengths. IEEE Transactions on Instrumentation and Measurement. 1992. Vol. 41, Iss. 5. Р. 723–725. https://doi.org/10.1109/19.177352
6. Kim S., Novotny D., Gordon J. A., Guerrieri J. R. A Free-Space Measurement Method for the Low-Loss Dielectric Characterization Without Prior Need for Sample Thickness Data. IEEE Transactions on Antennas and Propagation. 2016. Vol. 64, Iss. 9. Р. 3869–3879. https://doi.org/10.1109/tap.2016.2587745
7. Hehenberger S. P., Caizzone S., Thurner S., Yarovoy A. G. Broadband Eff ective Permittivity Simulation and Measurement Techniques for 3-D-Printed Dielectric Crystals. IEEE Transactions on Microwave Theory and Techniques. 2023. Vol. 71, Iss. 10. Р. 4161–4172. https://doi.org/10.1109/tmtt.2023.3259479.

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]]> 3.1.2025 Experimental research on separation diaphragm performance in propellant storage and feed systems of liquid propellant tanks https://journal.yuzhnoye.com/content_2025_1-en/annot_3_1_2025-en/ Wed, 27 Aug 2025 12:40:38 +0000 https://journal.yuzhnoye.com/?page_id=35481
Key words: Strength parameters; aircraft , space and rocket technologies; design parameters; mathematical simulation; fuel tank; separation diafragm; autonomous bench testing; critical pressure Bibliography: 1. Strength parameters; aircraft , space and rocket technologies; design parameters; mathematical simulation; fuel tank; separation diafragm; autonomous bench testing; critical pressure .
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3. Experimental research on separation diaphragm performance in propellant storage and feed systems of liquid propellant tanks

ISSN: 2617-5525

e-ISSN: 2617-5533

Автори: Shulha V. A., Pidhainyi A. I., Mudrov D. S.

Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2025 (1); 19-27

DOI: https://doi.org/10.33136/stma2025.01.019

Language: Ukrainian

Annotation: This paper presents the results of comprehensive research on the operational performance of diaphragm separators utilized in the fuel storage and supply systems for liquid-propellant rocket engines (LPRE). The relevance of this study arises from the need to ensure the reliable separation of gas and liquid duringthe operation of aerospace systems under diff erent conditions. In this context, special attention is given to autonomous bench tests that enable the evaluation of the key performance parameters of diaphragms before integrating them into production models. The paper examines the shape transformation of spherical diaphragms under external loads, presents an analytical calculation of the initial diaphragm inversion radius, and identifi es the critical pressures that cause buckling. The results of this calculation demonstrate a satisfactory correlation with the experimental data obtained during testing. The methodology for qualifi cation tests conducted on fi ve diff erent diaphragm variants is described. Several technological and design measures have been implemented to enhance product quality. They included increasing the number of drawing passes from two to three with intermediate annealing, reducing the thickness of the blanks, and enlarging the non-rolled polar zone. It was found that the primary factor ensuring defect-free diaphragm inversion is the reduced number of roller passings along the diaphragm contour, which prevents the tearing of the surface layer. The test results for diff erent diaphragm variants confi rmed satisfactory performance. An analysis of pressure diff erentials across the diaphragms during inversion confi rmed compliance with the technical specifi cations. The study concluded that the diaphragm design, when it incorporates all corrective measures, ensures defect-free inversion while maintaining the required pressure diff erential and is recommended for further testing as part of standard tank assemblies.

Key words: Strength parameters; aircraft, space and rocket technologies; design parameters; mathematical simulation; fuel tank; separation diafragm; autonomous bench testing; critical pressure

Bibliography:

1. Ballinger I. A., Lay W. D., Tam W. H. Review and History of PSI Elastomeric Diaphragm Tanks. 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 10-12
July 1995, San Diego, CA, USA. DOI: https://doi.org/10.2514/6.1995-2534.

2. Hartwig J. W. A detailed historical review of propellant management devices for low gravity propellant acquisition. 52nd AIAA/SAE/ASEE Joint Propulsion Conference,
25-27 July 2016, Salt Lake City, USA. Reston: American Institute of Aeronautics and Astronautics. DOI: https://doi.org/10.2514/6.2016-4772.

3. Lenahen B., Gangadharan S., Desai M. A Computational and Experimental Analysis of Spacecraft Propellant Tanks Implemented with Flexible Diaphragms. Proceedings of
the 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Boston, Massachusetts, USA: American Institute of Aeronautics and
Astronautics. DOI: https://doi.org/10.2514/6.2013-1886.

4. Sabaghzadeh H., Shafaee M. Reversal modeling and optimal design of hyper-elastic diaphragm in space fuel tanks. SN Applied Sciences. 2021. Vol. 3, Article number:
792. DOI: https://doi.org/10.1007/s42452-021-04785-0

5. Conomos H. A., Alongi C. G., Moore J., Yager J., Goddard R., Salzler T., Fetes J., Burch K. Development of 10 inch Diameter Titanium Rolling Metal Diaphragm Tank
for Green Propellant. AIAA Propellant Storage and Management II. DOI: https://doi.org/10.2514/6.2017-4915.

6. Jøraholmen T., Korsvold S., Sandvold P., Luktvasslimo Ø., Snilsberg K. E.
Roadmap towards a qualified aluminium green propellant diaphragm tank. Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS, 9-13 July 2023, Lausanne, Switzerland.
Lausanne: EUCASS. DOI: https://doi.org/10.13009/EUCASS2023-093.

7. Shen Y. A computational analysis of reversal behaviors of a spacecraft propellant management device. International Conference Optoelectronic Information and Optical
Engineering (OIOE 2024), 2024, Wuhan, China. Bellingham: SPIE, 2025. (Proceedings of SPIE; Vol. 13513). DOI: https://doi.org/10.1117/12.3045569.

8. Windisch M., Beck R. Numerical Simulation and Optimisation of a Hemisсherical Metallic Membrane Designed for Positive Expulsion of a Propellant Tank (for
Replacement of Conventional PMD). Spacecraft Structures, Materials and Mechanical Testing: Proceedings of a European Conference, 4-6 November 1998, Braunschweig,
Germany. Paris: European Space Agency (ESA), 1999. Vol. 428. P. 45. ISBN 9290927127.

9. Mudrov D.S., Zil V.V. Doslidzhennia napruzheno-deformovanoho stanu vytysknykh diafrahm. Heotekhnichna mekhanika: zb. nauk. prats. / In-t heotekh. mekh. im. M.S.
Poliakova NAN Ukrainy. Dnipro, 2016. Vyp. 131. S. 173-182.

10. Mozharovskii M.S. Teoriia pruzhnosti, plastychnosti i povzuchosti: pidruchnyk / M.S. Mozharovskyi. K. : Vyshcha shkola, 2002. 308 s.

11. Libai A., Simmonds J.G. The Nonlinear Theory of Elastic Shells. 2nd ed. Cambridge: Cambridge University Press, 1998. 564 p. ISBN 978-0-521-01976-7.

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3.1.2025 Experimental research on separation diaphragm performance in propellant storage and feed systems of liquid propellant tanks
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3.1.2025 Experimental research on separation diaphragm performance in propellant storage and feed systems of liquid propellant tanks

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]]> 2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop https://journal.yuzhnoye.com/content_2018_1-en/annot_2_1_2018-en/ Mon, 04 Sep 2023 12:45:06 +0000 https://journal.yuzhnoye.com/?page_id=30403
Energy-Intensive Fuels for Aircraft and Rocket Engines / Under the editorship of L. Zenit Space Launch System from the Eyes of its Developers / Under the editorship of e.d. Space Rocketry Ground Infrastructure Technological Facilities: Engineering Manual. Investigation of Prospective Propellant Preparation Technologies: Scientific-Technical Report 21.18258.173ОТ / Yuzhnoye SDO. Prospective Technologies to Prepare Propellants with Improved Performance Properties. Space technology. Space technology. Space technology. Space technology.
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2. Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop

ISSN: 2617-5525

e-ISSN: 2617-5533

Authors:

Salo М. P., Tereschenko K. O., Ivanitsky G. М.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2018 (1); 6-12

DOI: https://doi.org/10.33136/stma2018.01.006

Language: Russian

Annotation: An alternative method of kerosene dehydration is proposed, which is based on application of cyclic technology of supersaturation decrease using dry nitrogen. A comparison of nitrogen and time specific consumption in dehydration operations is done and recommendations are given for their use in the cosmodromes’ launch complexes fuel storage and preparation facilities.

Key words:

Bibliography:

1. Zrelov V. N., Seryogin E. P. Liquid Rocket Propellants. М., 1975. 320 p.
2. Energy-Intensive Fuels for Aircraft and Rocket Engines / Under the editorship of L. S. Yanovsky. М., 2009. 400 p.
3. Soyuz-2. URL: https://ru.wikipedia.org/wiki/Soyuz-2_(launch vehicle family).
4. Angara. URL: https://ru.wikipedia.org/wiki/Angara_(launch vehicle).
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6. Leshchiner L. B., Ul’yanov I. E. Designing of Aircraft Fuel Systems. М., 1975. 344 p.
7. Zenit Space Launch System from the Eyes of its Developers / Under the editorship of e.d. professor V. N. Solov’yov, e.d. professor G. P. Biryukov, N. S. Kozhukhov, N. I. Kursenkova. М., 2003. 213 p.
8. Space Rocketry Ground Infrastructure Technological Facilities: Engineering Manual. Book 1. М., 2005. 416 p.
9. Investigation of Prospective Propellant Preparation Technologies: Scientific-Technical Report 21.18258.173ОТ / Yuzhnoye SDO. 2016. 115 p.
10. Shleifer A. A., Litvinov A. N. Prospective Technologies to Prepare Propellants with Improved Performance Properties. Ul’yanovsk, 1989. 215 p.
11. Englin B. A. Use of Liquid Propellants at Low Temperatures. 3-rd edition revised and enlarged. М., 1980. 207 p.
12. Volkov A. I., Zharsky I. M. Big Chemical Guide. Minsk, 2005. 608 p.
13. Calculated Evaluation and Experimental Check of RPC Degassing and Saturation by Helium for Filling Cyclone-4 LV: Technical Note Cyclone-4. 22.6849.123 СТ / Yuzhnoye SDO. 2005. 29 p.

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