Article
Cover

Title
Creating a domestic platform for mathematical modelling and engineering analysis tools to solve practical problems related to the development and optimization of rocket and space technologiesAuthors
A.Sh. Kozaev, V.V. Mironov, A.S. Negodyaev, E.S. TsirendorzhievOrganization
JSC State Scientific Center of the Russian Federation “Keldysh Research Center”Moscow, The Russian Federation
Abstract
The purpose of the work is to create a domestic software platform for solving mathematical modeling problems in the industry. It is known that the most important task of reducing costs and meeting deadlines when creating new products is the development of advanced mathematical models which are quick-response enough and adequately approximate real processes. To solve this problem, the Keldysh Research Center has been implementing a number of projects aimed at the development of the domestic platform for the mathematical modeling and engineering analysis tools to provide practical issues for the development and optimization of parameters primarily for rocket engines and space power systems. A set of fundamental principles taken into account while developing the platform is formulated in the work. Firstly, this is the development and application of the only domestic software tools and complex solutions based on specialized software of Keldysh Research Center, as well as commercial domestic software products. Secondly, the integration of components into a single complex of mathematical models and software with automated calculations. Besides that, the validation of mathematical models and software created for modes and conditions of practical tasks to ensure a given accuracy. The authors provide examples of successful application of the developed platform in relation to the problems of development and optimization of spacecraft. At the moment, along with solving applied problems, the modeling results have already made it possible to formulate a number of practical recommendations, as well as to identify a number of new effects and physical patterns inherent in the complex technical devices considered.Keywords
mathematical modelling, engineering analysis, CAE, computational experiment, software, design automation, predictive modellingReferences
[1] Pogosyan M. A., Savelevskikh E. P., Shagaliev R. M., Kozelkov A. S., Strelets D. Yu., Ryabov A. A., Kornev A. V., Deryugin Yu.N., Spiridonov V. F., Tsiberev K. V. Application of Domestic Supercomputer Technologies for the Creation of Promising Samples of Aviation Equipment // VANT Journal, ser. Mathematical modelling of physical processes, 2013, No. 2, pp. 3–18.
[2] Ivanova T. G., Stryukov Ya. A., Berg D. A., Karakotin I. N. Prospects for the Implementation of the Logos Software Package and its Testing Methodology for Aerodynamic and Thermal Design of Launch Vehicles // XIV Korolyov readings: international youth scientific conference dedicated to the 110th anniversary of the birth of Academician S. P. Korolev, the 75th anniversary of KuAI-SGAU-SamSU-Samara University and the 60th anniversary of the launch of the first artificial Earth satellite: in 2 volumes, Samara, October 03–05, 2017. Volume 1. – Samara: Samara National Research University named after Academician S. P. Korolev, 2017. p. 198.
[3] Kornev A. V., Kozelkov A. S., The Use of Domestic Supercomputer Technologies to Create Promising Models of Aviation Equipment // Modern information technologies and IT education. 2021. vol. 17, No. 2. pp. 250–264
[4] Koshlakov V. V., Gotovtsev K. V., Zakharenkov L. E., Karevsky A. V., Kiryushin E. N., Lovtsov A. S., Oshev Yu.A., Semenkin A. V., Solodukhin A. E., Fedotov S. Yu., Fedyunin S. Yu., Tsvetkov A. G. The Experimental Bench Base of JSC “Keldysh Research Center” for Testing Powerful Power Propulsion Systems // Space engineering and technologies. 2022, No. 1(36), pp. 80–95.
[5] Abdullin M. F., Barabanov R. A., Kvaratskhelia D. D., Filimonkin E. A., Kitaev M. V., Kornev A. V., Nikitin M. V., Saganov E. B. The Logos Software Package. Functional Capabilities for Modelling Static Deformation of Layered Composite Materials Based on a Shell Finite Element // Journal of VANT, ser. Mathematical modelling of physical processes, 2020, No. 2, pp. 60–70.
[6] Modelling of Flight Dynamics of an Aircraft Taking into Account the Operation of the Power Systems and Controls / A. V. Sarazov, A. S. Kozelkov, A. A. Utkina, A. V. Kornev // Aerospace engineering, high technologies and innovations. 2022. Vol. 1. pp. 203–204.
[7] Ananyev A. V., Laptev I. V., Tsirendorzhiev E. S. A Thermal Model of a Thermocatalytic Engine on Hydrazine // Proceedings of the Eighth Russian National Conference on Heat Exchange: Proceedings of the Conference. In 2 volumes, Moscow, October 17–22, 2022. Vol. 1. Moscow: National Research University “MEI”, 2022. pp. 224–225.
[8] Certificate of State Registration of the Computer Program No. 2023667463 Russian Federation. The program for calculating the parameters of filtration combustion in the combustion chamber of the LRE Gorenje: No. 2023666617: application. 08/01/2023: publ. 08/15/2023 / A. V. Ananyev, A. A. Kuroedov, I. V. Laptev, E. S. Tsirendorzhiev; applicant Joint Stock Company State Scientific Center of the Russian Federation “Keldysh Research Center”.
[9] Kuroedov A. A., Cherkasov S. G., Laptev I. V., Moiseeva L. A. Condensation of Pressurized Gas in a Fuel Tank with a Separating Diaphragm in Zero Gravity // Thermal processes in engineering. 2021. vol. 13, No. 4. pp. 155–163.
[10] Petrova S. V., Gorodnov A. O., Laptev I. V. Model of Conjugate Heat Transfer in a Rocket Tank during Fuel Extraction with Simultaneous Supercharging // Problems of gas dynamics and heat and mass transfer in power systems: Abstracts of the XXIV school of the seminar of young scientists and specialists under the leadership of the Academy of Sciences. RAS A. I. Leontiev, dedicated to the 100th anniversary of Academician V. E. Alemasov, Kazan, May 23–27, 2023. Kazan: JSC Information and Publshing Center, 2023. pp. 256–257.
[11] Determination of conditions ensuring constant pressure of liquefied gas vapor in the fuel tank during external heat exchange and changing volume of the pressurized cavity / State Scientific Center FSUE “Keldysh Research Centre”. Executors are Ananyev A. V., Vasyutychev A. S., Gorodnov A. O. Inv. № . 7428, 2020, 70 p.
For citing this article
Kozaev A.Sh., Mironov V.V., Negodyaev A.S., Tsirendorzhiev E.S. Creating a domestic platform for mathematical modelling and engineering analysis tools to solve practical problems related to the development and optimization of rocket and space technologies // Spacecrafts & Technologies, 2024, vol. 8, no. 2, pp. 120-131.
This Article is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).