Applicability of Elastic Elements in the Problem of Stratification of a Transversely Composite Cryogenic Tank
Authors: Egorov A.V., Vasiliev F.Al.
Published in issue: #7(175)/2026
Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft
The delamination problem is solved based on a finite-element analysis of the stress-strain state of a cylindrical cryogenic tank reinforced with an external elastic mesh. It is assumed that the tank consists of two layers. The inner supporting layer is made of metal, while the outer thermal insulation layer is made of foam. During the cooling process, an undesirable gap forms between the layers, and this is proposed to be eliminated by using a stretched elastic mesh. The gap and the required tension force are evaluated by comparing the results of two calculations: one without the mesh and the other with the mesh. Given the axial symmetry of the tank design, a transversely composite thin-walled ring is chosen as the calculation scheme, which simulates the central cylindrical part of the tank. The loads are represented by the temperature, which cools the inner surface of the metal ring from a normal value to a cryogenic value over time, while the outer surface of the foam ring remains uncooled.
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References
[1] Ignatyev A.V. Razvitie metoda konechnykh elementov v forme klassicheskogo smeshannogo metoda stroitelnoy mekhaniki: Dis. … d-ra tekhn. nauk: 05.23.17 [Development of the finite element method in the form of the classical mixed method of structural mechanics: Diss. … Dr. Sc. (Engineering): 05.23.17]. Volgograd, 2019, 294 p.
[2] Orlov V.G., Scherbakova T.N., Telegin S.V., Malkov V.V., Aleksandrov N.G. Paket teplovoy izolyatsii i sposob ego izgotovleniya [Thermal insulation package and method of its manufacturing]. Pat. No. 2459743 C1, Russian Federation, 2012, Bull. no. 24, 7 p.
[3] Zaletayev S.V., Kopyatkevich R.M. Programmnyy kompleks teplovogo proektirovaniya i analiza teplovykh rezhimov kosmicheskikh apparatov [Software complex for thermal design and analysis of thermal regimes of spacecraft]. Kosmonavtika i raketostroenie — Cosmonautics and Rocket Engineering, 2014, no. 4 (77), pp. 84–91.
[4] Popov A.N. Modelirovanie konstruktivno-nelineynykh kontaktnykh zadach v programmnom komplekse ANSYS [Modeling of structural nonlinear contact problems in the ANSYS software complex]. Forum molodezhnoy nauki, 2021, iss. 2, no. 2, pp. 4–10.
[5] Opisanie razrabatyvaemogo kislorodno-vodorodnogo razgonnogo bloka [Description of the developed oxygen–hydrogen upper stage]. Khrunichev Space Research and Production Center. Available at: http://www.khrunichev.ru/main.php?id=52 (accessed February 26, 2026).
[6] Mishin V.P., Karrask V.K., eds. Osnovy konstruirovaniya raket-nositeley kosmicheskikh apparatov [Fundamentals of launch vehicle design]. Moscow, Mashinostroenie Publ., 1991, 416 p.
[7] Kablov E.N. Konstruktsionnye kompozitsionnye materialy [Structural composite materials]. Moscow, VIAM Publ., 2012, 58 p.
[8] Scherbakova T.N., Serezhenkova V.V., Yanshin Kh.Ya., Kudryashova N.V., Savvateeva O.A. Mnogosloynoe izdelie i sposob ego izgotovleniya (varianty) [Multilayer product and method of its manufacturing (variants)]. Pat. No. 2298480, Russian Federation, 2007, Bull. no. 13, 9 p.
[9] Opisanie konstruktsii i ekspluatatsii bloka Ts RN “Energiya” [Description of the design and operation of the central unit of the Energia launch vehicle]. Buran.ru. Available at: http://www.buran.ru/htm/15-3.htm (accessed February 21, 2026).
[10] Kasymov U.T., Tolebay S.A., Berik M.B. Sistema zapravki rakety-nositelya s trekhkomponentnymi zhidkostnymi raketnymi dvigatelyami [Propellant loading system for a launch vehicle with three-component liquid rocket engines]. In: IV Mezhdunarodnaya nauchno-prakticheskaya konferentsiya studentov, aspirantov, prepodavateley “Prikladnye voprosy tochnykh nauk” [IV International Scientific and Practical Conference of Students, Postgraduates and Teachers “Applied Problems of Exact Sciences”]. November 13–14, Armavir, Armavir State Pedagogical University, 2020, pp. 51–54.
[11] Basov K.A. ANSYS v primerakh i zadachakh [ANSYS in examples and problems]. Moscow, KompyuterPress Publ., 2002, 224 p.
[12] Balabukh L.I., Alfutov N.A., Usyukin V.I. Stroitelnaya mekhanika raket [Structural mechanics of rockets]. Moscow, HSE Publ., 1984, 391 p.