| タイトル | Design and Analysis of a Turbopump for a Conceptual Expander Cycle Upper-Stage Engine |
| 本文（外部サイト） | http://hdl.handle.net/2060/20060047641 |
| 著者（英） | Forbes, John C.; Dorney, Daniel J.; Huber, Frank W.; Griffin, Lisa W.; Thornton, Randall J.; Rothermel, Jeffry; Skelly, Stephen E. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2006-01-01 |
| 言語 | eng |
| 内容記述 | As part of the development of technologies for rocket engines that will power spacecraft to the Moon and Mars, a program was initiated to develop a conceptual upper stage engine with wide flow range capability. The resulting expander cycle engine design employs a radial turbine to allow higher pump speeds and efficiencies. In this paper, the design and analysis of the pump section of the engine are discussed. One-dimensional meanline analyses and three-dimensional unsteady computational fluid dynamics simulations were performed for the pump stage. Configurations with both vaneless and vaned diffusers were investigated. Both the meanline analysis and computational predictions show that the pump will meet the performance objectives. Additional details describing the development of a water flow facility test are also presented. |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| レポートNO | FEDMS2006-98101 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
