Abstract
On the base of the simplified analytical model for the bimetallic shell of the combustion chamber of the reusable liquid-propellant rocket engine, the analysis of the loading of connectors between the shell walls and the accumulation of inelastic deformations in the inner wall material was carried out. The results obtained can be used for evaluation of the maximal number of engine operation cycles.
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Original Russian Text © V.S. Zarubin, V.N. Zimin, G.N. Kuvyrkin, 2018, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2018, No. 3, pp. 100–107.
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Zarubin, V.S., Zimin, V.N. & Kuvyrkin, G.N. Estimation of the Combustion Chamber Shell Working Capacity for the Reusable Liquid-Propellant Rocket Engine. Russ. Aeronaut. 61, 425–433 (2018). https://doi.org/10.3103/S1068799818030169
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DOI: https://doi.org/10.3103/S1068799818030169