Estimation of the Combustion Chamber Shell Working Capacity for the Reusable Liquid-Propellant Rocket Engine
- Авторы: Zarubin V.S.1, Zimin V.N.1, Kuvyrkin G.N.1
-
Учреждения:
- Bauman Moscow State Technical University
- Выпуск: Том 61, № 3 (2018)
- Страницы: 425-433
- Раздел: 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
Цитировать
Аннотация
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.
Ключевые слова
Об авторах
V. Zarubin
Bauman Moscow State Technical University
Email: Fn2@bmstu.ru
Россия, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
V. Zimin
Bauman Moscow State Technical University
Email: Fn2@bmstu.ru
Россия, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
G. Kuvyrkin
Bauman Moscow State Technical University
Автор, ответственный за переписку.
Email: Fn2@bmstu.ru
Россия, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
Дополнительные файлы
