タイトル | Turbopump radial and axial rotor support system |
本文(外部サイト) | http://hdl.handle.net/2060/19720000264 |
著者(英) | Buckmann, P. S. |
著者所属(英) | NASA Marshall Space Flight Center |
発行日 | 1972-06-01 |
言語 | eng |
内容記述 | Design of thrust balancer minimizes leakage bypass and obviates need for conventional thrust balancer. System allows operation at low flow rates and high thrust capacity at cryogenic temperatures and high pressures. |
NASA分類 | MACHINERY |
レポートNO | 72B10264 MFS-21495 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/500908 |