A method for reducing dynamic loads during switching stages of multistage hydraulic cylinders of launch vehicles rising drive

Author:

lgritskaia A.,Zabegaev A.,Zverev V.,lgritsky V.

Publisher

AIP Publishing

Reference26 articles.

1. Dynamic analysis of non-linear processes in super heavy-lift launch vehicle erector and polyspast lifting system

2. Prospects of using electromechanical drives based on roller screw mechanisms in aerospace hardware

3. New design of gapless planetary roller screw mechanism

4. Hydraulic Lifting Mechanisms for the Erection Equipment

5. Zverev V.A., Igritskaya A.Yu., Igritsky V.A. The methodology of graphic-analytical calculation of the optimal geometric parameters of hydraulic drives for lifting ILVs // Actual problems of astronautics: XLIII Academic readings in astronautics dedicated to the memory of academician S.P. Korolev and other prominent domestic scientists - pioneers of space exploration (Moscow, January 29 - February 1, 2019): abstract: 2 volumes - T. 1. - M.: BMSTU Publishing House, 2019 .-- 419 p. - ISBN 978-5-7038-5094-7. (in Russian)

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1. Numerical modeling practice for aircraft flow control problems;AIP Conference Proceedings;2023

2. An effectiveness analysis of reducing inertial loads acting on space rockets during the stages switching of lift cylinders by mounting them at different initial angles;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

3. A design constraint for a double-acting telescopic hydraulic cylinder in a hydraulic erecting system;Journal of Zhejiang University-SCIENCE A;2022-01

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