| タイトル | Two phase pumping of cryogenic propellants |
| 著者（英） | Gross, L. A.; Stinson, H. P. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1972-08-01 |
| 言語 | eng |
| 内容記述 | Two-phase cryogenic propellant pumping techniques developed during the past 5 years are discussed. During this period the theory of two-phase pumping of hydrogen was developed into an operational technique that can result in significant benefits to space vehicle propulsion systems. Using two-phase pumping techniques, zero LH2 tank net positive suction head (NPSH) was demonstrated on turbopump and rocket engine firings, and limited experimental results show that two-phase pumping of liquid oxygen is feasible. Design techniques were developed for improving the two-phase pumping capability of inducers. |
| NASA分類 | PROPELLANTS |
| レポートNO | 73N12843 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/533683 |
