| タイトル | Liquid rocket engine axial-flow turbopumps |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780023221 |
| 著者（英） | Scheer, D. D.; Farquhar, J.; Keller, R. B., Jr.; Viteri, F.; Huppert, M. C. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1978-04-01 |
| 言語 | eng |
| 内容記述 | The axial pump is considered in terms of the total turbopump assembly. Stage hydrodynamic design, pump rotor assembly, pump materials for liquid hydrogen applications, and safety factors as utilized in state of the art pumps are among the topics discussed. Axial pump applications are included. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 78N31164
NASA-SP-8125 |
| 権利 | No Copyright |
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