http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
1 online resource (1 online resource (158 pages)).
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.
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.
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Society of Automotive Engineers. Electronic publications