| タイトル | Chilldown study of the single stage inducer test rig |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730015551 |
| 著者（英） | Kimura, L. A. |
| 著者所属（英） | Aerojet Nuclear Systems Co. |
| 発行日 | 1972-06-02 |
| 言語 | eng |
| 内容記述 | Of the six chilldown tests, data from only one could be used for evaluation. During the rest of the chilldown tests, there was leakage hydrogen flow into the pump cavity prior to the initiation of the chilldown test. In all of the tests the hydrogen condition into the pump was probably 100% vapor. The data from this one test, therefore, can be used to compare only the single phase fluid correlation in the analytical pump chilldown model. In general, the actual pump chilled down much faster than predicted by the analytical pump model. There were insufficient data from the test to measure the pump flow rate and pump inlet fluid condition; therefore, these parameters were extrapolated based on related data which were available. However, even with the highest probable flow rate, the pump chilled faster than predicted. |
| NASA分類 | FACILITIES, RESEARCH, AND SUPPORT |
| レポートNO | 73N24278
N8110R:72-033
NASA-CR-132212 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/199109 |
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