电邮这篇文章 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
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隶属关系:
- 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.
作者简介
V. Zarubin
Bauman Moscow State Technical University
Email: Fn2@bmstu.ru
俄罗斯联邦, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
V. Zimin
Bauman Moscow State Technical University
Email: Fn2@bmstu.ru
俄罗斯联邦, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
G. Kuvyrkin
Bauman Moscow State Technical University
编辑信件的主要联系方式.
Email: Fn2@bmstu.ru
俄罗斯联邦, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
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