Analysis of the dynamic operating modes of the verticalization system of the universal launch complex for a promising super-heavy ILV
Authors: Zotov V.G., Nikitin A.O., Yazykov A.V.
Published in issue: #8(116)/2021
DOI: 10.18698/2308-6033-2021-8-2103
Category: Aviation and Rocket-Space Engineering | Chapter: Ground Complexes, Launch Equipment, Aircraft Exploitation
The paper presents the results of the analysis of the dynamic processes occurring at different stages of the operation of the installation unit of the super-heavy-class space rocket complex for one of the options for completing the Yenisei space rocket, intended for both the implementation of the lunar program and deep space exploration. Verticalization and installation of the ILV under consideration on the launch pad is carried out by a lifting and installation unit of an original design. The main feature of this unit is the presence of two tilting axes. The considered type of installation unit has not previously been used in domestic complexes for ILV. Despite some similarities of such a unit with a classic installer with lifting frame, in the course of its operation, specific operating modes arise with increased dynamic loading of the unit structure and the lifted product. The calculations made it possible to propose constructive solutions that ensure a decrease in dynamic loads on a space rocket during verticalization and installation on a launch pad.
References
[1] NTS po kosmicheskomu raketnomu kompleksu sverkhtyazhelogo klassa [Scientific and Technical Council on the space rocket complex of the super-heavy class]. Available at: https://www.roscosmos.ru/27720/ (accessed January 21, 2021).
[2] Didkovsky A.A., Mukhina E.D., Chernov A.K. Vestnik Permskogo natsional’nogo issledovatel’skogo politekhnicheskogo universiteta. Aerokosmicheskaya tekhnika — Bulletin of the Perm National Research Polytechnic University. Aerospace engineering, 2020, no. 63, pp. 23–29. DOI: 10.15593/2224-9982/2020.63.03
[3] Sutyrina O.A., Yazykov A.V. Investigation of the issues of platform motion for vertical transportation of promising super-heavy ILVs. In: XL Academic Readings in Cosmonautics: a collection of abstracts. Moscow, January 26–29, 2016. Moscow, Bauman Moscow State Technical University, 2015, pp. 242–243.
[4] Ivanov A.G., Igritskiy V.A. On the possibilities of using tracked chassis for the transportation of promising super-heavy space rockets. In: XLIV Academic Readings on Cosmonautics: a collection of abstracts. Moscow, January 28–31, 2020. In 2 volumes. Moscow, BMSTU Press, 2020, vol. 1, pp. 642–644.
[5] Udovik I.S., Zolin A.V. Inzhenerny zhurnal: nauka i innovatsii — Engineering Journal: Science and Innovation, 2020, iss. 7 (103), p. 7. DOI: 10.18698/2308-6033-2020-7-1998
[6] Igritskiy V.A. On the numerical assessment of the convenience of servicing super-heavy space rockets and their elements with horizontal and vertical variants of their preparation technology. In: XLIII Academic Readings on Cosmonautics: Collection of abstract. Moscow, BMSTU Press, 2019, pp. 329–330.
[7] Barmin I.V., ed. Tekhnologicheskiye ob"yekty nazemnoy infrastruktury raketno-kosmicheskoy tekhniki [Technological objects of ground infrastructure of rocket and space technology]. (Engineering manual). Book 2. Moscow, 2006.
[8] Biryukov G.P., Manaenkov E.N., Levin B.K. Tekhnologicheskoye oborudovaniye otechestvennykh raketno-kosmicheskikh kompleksov [Technological equipment of domestic rocket and space complexes]. Fadeev A.S., Torpachev A.V., eds. Moscow, Restart Publ., 2011, 600 p.
[9] Abakumov V.S., Zverev V.A., Lomakin V.V., Chugunkov V.V., Yazykov A.V. Vestnik Moskovskogo gosudarstvennogo tekhnicheskogo universiteta imeni N.E. Baumana. Ser. Mashinostroyeniye — Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, 2008, Special iss., pp. 124–130.
[10] Zverev V.A., Lomakin V.V., Yazykov A.V. Nauka i obrazovaniye: nauchnoye izdaniye MGTU im. N.E. Baumana — Science and Education: scientific journal of the Bauman Moscow State Technical University, 2013, no. 3, pp. 179–190.