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Liquid rocket engine thrust chamber : parametrical modeling /

This book presents an innovative parametric model applicable to the project of some elements of the liquid rocket thrust chamber with the level of detail and accuracy appropriate to the preliminary design phase. It addresses the operating characteristics and dimensioning of some thrust chamber eleme...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Rezende, Rene Nardi
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Warrendale, Pa. (400 Commonwealth Dr., Warrendale PA USA) : Society of Automotive Engineers, 2018.
Colección:Society of Automotive Engineers. Electronic publications
Temas:
Acceso en línea:Texto completo
Descripción
Sumario:This book presents an innovative parametric model applicable to the project of some elements of the liquid rocket thrust chamber with the level of detail and accuracy appropriate to the preliminary design phase. It addresses the operating characteristics and dimensioning of some thrust chamber elements through a set of equations and parameters, which include thrust or propellant characteristics. The model degree of sophistication was adjusted to the requirements of the Project Life Cycle Phase B, while also enabling quick analysis of new configurations from changes in initial project parameters.
Notas:Title from PDF title page (SAE Web site, 01/15/2019)
Descripción Física:1 online resource (1 PDF (158 pages))
Bibliografía:Includes bibliographical references.
ISBN:9780768095425
0768095425
9780768093346
0768093341
9780768093339
0768093333
9780768093353
076809335X
9781523124152
1523124156