| タイトル | Hydrostatic lift-off seal |
| 著者（英） | Buckmann, P. S. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1976-03-01 |
| 言語 | eng |
| 内容記述 | Interpropellant turbopump oxidizer seal consists of smooth flat surface on back of second-stage oxidizer impeller, floating seal ring, semistatic piston ring secondary seal, and low pressure flexible-bellows static secondary seal. Seal performs static sealing at rest and controlled leakage sealing in operation. |
| NASA分類 | MECHANICS |
| レポートNO | 76B10079
MFS-21496 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/446139 |
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