Estimation of the Combustion Chamber Shell Working Capacity for the Reusable Liquid-Propellant Rocket Engine

V. S. Zarubin; V. N. Zimin; G. N. Kuvyrkin

doi:10.3103/S1068799818030169

Estimation of the Combustion Chamber Shell Working Capacity for the Reusable Liquid-Propellant Rocket Engine

作者: Zarubin V.S.¹, Zimin V.N.¹, Kuvyrkin G.N.¹
隶属关系:
1. Bauman Moscow State Technical University
期: 卷 61, 编号 3 (2018)
页面: 425-433
栏目: Aircraft and Rocket Engine Design and Development
URL: https://journals.rcsi.science/1068-7998/article/view/230626
DOI: https://doi.org/10.3103/S1068799818030169
ID: 230626

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详细

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.