Email this article Estimation of the Combustion Chamber Shell Working Capacity for the Reusable Liquid-Propellant Rocket Engine
- Authors: Zarubin V.S.1, Zimin V.N.1, Kuvyrkin G.N.1
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Affiliations:
- Bauman Moscow State Technical University
- Issue: Vol 61, No 3 (2018)
- Pages: 425-433
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journal-vniispk.ru/1068-7998/article/view/230626
- DOI: https://doi.org/10.3103/S1068799818030169
- ID: 230626
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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.
About the authors
V. S. Zarubin
Bauman Moscow State Technical University
Email: Fn2@bmstu.ru
Russian Federation, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
V. N. Zimin
Bauman Moscow State Technical University
Email: Fn2@bmstu.ru
Russian Federation, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
G. N. Kuvyrkin
Bauman Moscow State Technical University
Author for correspondence.
Email: Fn2@bmstu.ru
Russian Federation, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
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