Comprehensive Approach to Verification in Design and Development of the Antenna Head Fairing Body

Abstract

Design of complex technical systems in the rocket and space applications requires using the solutions aimed at achieving the specified operation objectives, acceptable financial and economic design results and the required reliability indicators of the products. To achieve the optimal design result, it is necessary to verify comprehensively the design solutions. The paper considers combined application of the theory of solving the inventive problems, functional cost analysis, and design and technological reliability analysis as one of the approaches to verification. Functional analysis lies in the basis of implementing all the three methods; it helps to represent the design as a set of the required functions. This technique makes it possible to abstract from the design solutions and describe any design in a form convenient for analysis enabling the designer to find acceptable solutions in achieving the product operation objectives, optimizing the costs, and justifying the specified requirements to ensure operability and reliability. Results of each analysis technique could serve as a reason for conducting the design procedures iterative cycle to achieve optimal results in design and development. The paper presents results of comprehensive verification of the design and development solutions using an example of the aircraft antenna radio-transparent head fairing body

Please cite this article in English as:

Pokhabov Yu.P., Kaverin V.A., Saparbaeva E.R., et al. Comprehensive approach to verification in design and development of the antenna head fairing body. Herald of the Bauman Moscow State Technical University, Series Mechanical Engineering, 2025, no. 3 (154), pp. 54--70 (in Russ.). EDN: SGSHCI

References

[1] Conley P.L. Space vehicle mechanisms. New York, John Wiley & Sons, 1998.

[2] Jones J.C. Design methods. New York, John Wiley & Sons, 1982.

[3] Roth K. Konstruieren Mit Konstruktionskatalogen. Berlin, Springer-Verlag, 1994.

[4] Krause W. Geratekonstruktion. Berlin, VEB Verlag-Technik, 1982.

[5] Dietrych J. System i konstrukcja. Warszawa, Wydawnictwa Naukowo-Techniczne, 1978.

[6] Kaplun V.A. Obtekateli antenn SVCh [Microwave antenna fairings]. Moscow, Sovetskoe radio Publ., 1974.

[7] Zhidkova O.G., Borodavin A.V., Mityushkina D.V., et al. Designing of radio-transparent constructions from composite materials. Konstruktsii iz kompozitsionnykh materialov [Composite Materials Constructions], 2020, no. 1, pp. 6--12 (in Russ.).

[8] Altshuller G. The innovation algorithm. Worcester, Technical Innovation Center, 1999.

[9] Chyapyale Yu.M. Metody poiska izobretatelskikh idey [Methods for searching for inventive ideas]. Leningrad, Mashinostroenie Publ., 1990.

[10] Konovalov A.A. Logika izobreteniya [Logic of invention]. Izhevsk, Udmurtiya Publ., 1990.

[11] Goldovskiy B.I., Vaynerman M.I. Kompleksnyy metod poiska resheniy tekhnicheskikh problem [A comprehensive method for solving technical problems]. Moscow, Rechnoy transport Publ., 1990.

[12] Ershova I.V., Prilutskaya M.A., Murukina A.D. Modernization of the method of functional and cost analysis in the conditions of digital transformation of industry. Organizator proizvodstva [Production Organizer], 2021, vol. 29, no. 4, pp. 35--47 (in Russ.). DOI: https://doi.org/10.36622/VSTU.2021.15.23.004

[13] Golibardov E.I., Kudryavtsev A.V., Sinenko M.I. Tekhnika FSA [FSA technique]. Kiev, Tekhnika Publ., 1989.

[14] Moiseeva N.K. Funktsionalno-stoimostnoy analiz v mashinostroenii [Functional and cost analysis in mechanical engineering]. Moscow, Mashinostroenie Publ., 1987.

[15] Pokhabov Yu.P. Teoriya i praktika obespecheniya nadezhnosti mekhanicheskikh ustroystv odnorazovogo srabatyvaniya [Theory and practice of ensuring the reliability of single-use mechanical devices]. Krasnoyarsk, SFU Publ., 2018.

[16] Pokhabov Yu.P. Method for designing and developing space mechanisms with specified dependability. Nadezhnost [Dependability], 2023, vol. 23, no. 2, pp. 26--38 (in Russ.). DOI: https://doi.org/10.21683/1729-2646-2023-23-2-26-38

[17] Pokhabov Yu.P., Kaverin V.A., Belov M.V., et al. Results of reliability design and technological analysis of the nose fairing pusher. Inzhenernyy zhurnal: nauka i innovatsii [Engineering Journal: Science and Innovation], 2023, no. 5 (in Russ.).DOI: https://doi.org/10.18698/2308-6033-2023-5-2273

[18] Pokhabov Yu.P. Certain conclusions on results of introducing the reliability design and technological analysis in rocket and space production. Part 1. Inzhenernyy zhurnal: nauka i innovatsii [Engineering Journal: Science and Innovation], 2023, no. 8 (in Russ.). DOI: https://doi.org/10.18698/2308-6033-2023-8-2297

[19] Pokhabov Yu.P. Certain conclusions on results of introducing the reliability design and technological analysis in rocket and space production. Part 2. Inzhenernyy zhurnal: nauka i innovatsii [Engineering Journal: Science and Innovation], 2023, no. 9 (in Russ.). DOI: https://doi.org/10.18698/2308-6033-2023-9-2304

[20] Svetlov V.G., Filippov V.S., Minokin L.M., et al. Sistema "Antenna--obtekatel" ["Antenna-dome" system]. Patent RU 2096869. Appl. 17.05.1996, publ. 20.11.1997 (in Russ.).

[21] Dergachev A.A., Kaverin V.A., Nalitkin O.N., et al. Korpus golovnogo antennogo obtekatelya letatelnogo apparata i sposob ego sborki [Aircraft head antenna radome housing and method of its assembly]. Patent RU 2823544. Appl. 09.10.2023, publ. 24.07.2024 (in Russ.).