Method of calculating the thickness of the combustion chamber of a liquid rocket engine made with the use of innovative technologies and materials
The use of innovative techniques in the production of parts and assembly units is one of the promising trends connected with increasing mass-energy characteristics of liquid- propellant jet engines. The article presents a concept of development of a liquid-propellant jet engine combustion chamber wi...
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| Format: | Article |
| Language: | English |
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Samara National Research University
2016-12-01
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| Series: | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
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| Online Access: | https://journals.ssau.ru/vestnik/article/viewFile/3308/3210 |