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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...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| 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 |
MARC
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| 003 | OCoLC | ||
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| 020 | |a 9781523124152 |q (electronic bk.) | ||
| 020 | |a 1523124156 |q (electronic bk.) | ||
| 020 | |z 9780768093322 |q (print) | ||
| 024 | 7 | |a 10.4271/0768093333 |2 doi | |
| 035 | |a (OCoLC)1082885850 | ||
| 050 | 4 | |a TL782 |b .R49 2018eb | |
| 082 | 0 | 4 | |a 629.47/5 |2 23 |
| 049 | |a UAMI | ||
| 100 | 1 | |a Rezende, Rene Nardi, | |
| 245 | 1 | 0 | |a Liquid rocket engine thrust chamber : |b parametrical modeling / |c Rene Nardi Rezende. |
| 264 | 1 | |a Warrendale, Pa. (400 Commonwealth Dr., Warrendale PA USA) : |b Society of Automotive Engineers, |c 2018. | |
| 300 | |a 1 online resource (1 PDF (158 pages)) | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a electronic |b txt |2 isbdmedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a Society of Automotive Engineers. Electronic publications | |
| 504 | |a Includes bibliographical references. | ||
| 505 | 0 | |a Chapter 1. Introduction -- Chapter 2. Fundamentals of rcket populsion -- Chapter 3. Methodology -- Chapter 4. Thrust chamber performance assessment -- Chapter 5. Nozzle dimensioning -- Chapter 6. Combustion chamber dimensioning -- Chapter 7. Nozzle configuration -- Chapter 8. Complementing the performance calculation -- Chapter 9. The cold section -- Chapter 10. The simplex swirl injector -- Chapter 11. The Pintle injector -- Appendix. | |
| 520 | |a 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. | ||
| 500 | |a Title from PDF title page (SAE Web site, 01/15/2019) | ||
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Space vehicles |x Propulsion systems. | |
| 650 | 0 | |a Rockets (Aeronautics) | |
| 650 | 6 | |a Véhicules spatiaux |x Propulsion. | |
| 650 | 6 | |a Fusées (Aéronautique) | |
| 650 | 7 | |a TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics. |2 bisacsh | |
| 650 | 7 | |a Rockets (Aeronautics) |2 fast | |
| 650 | 7 | |a Space vehicles |x Propulsion systems |2 fast | |
| 710 | 2 | |a Society of Automotive Engineers, |e publisher. | |
| 776 | 0 | 8 | |i Print version: |z 9780768093322 |w (DLC) 2018940787 |
| 810 | 2 | |a Society of Automotive Engineers. |t Electronic publications. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpLRETCPM7/toc |z Texto completo |
| 938 | |a SAE International |b PASA |n 9780768095425 | ||
| 938 | |a YBP Library Services |b YANK |n 17853496 | ||
| 938 | |a IEEE |b IEEE |n 8854942 | ||
| 938 | |a YBP Library Services |b YANK |n 302472976 | ||
| 994 | |a 92 |b IZTAP | ||