The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies

The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies

Some data on the knowledge base to support the development of low-thrust liquid-propellant rocket engines using computer technologies are presented. The structure of the base is proposed on the basis of characteristic features of engines, including the purpose, fuel components, physical principles o...

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Bibliographic Details
Main Author: V. V. Ryzhkov
Format: Article
Language:English
Published: Samara National Research University 2022-01-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
knowledge base
low-thrust rocket engine
mathematical models
graphic packages
electronic versions of engineering solutions
engines based on various physical principles
forms of communications with the knowledge base
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/10017/8853

Internet

https://journals.ssau.ru/vestnik/article/viewFile/10017/8853

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