| タイトル | Uranium droplet core nuclear rocket |
| 著者（英） | Anghaie, Samim |
| 著者所属（英） | Florida Univ. |
| 発行日 | 1991-09-01 |
| 言語 | eng |
| 内容記述 | Uranium droplet nuclear rocket is conceptually designed to utilize the broad temperature range ofthe liquid phase of metallic uranium in droplet configuration which maximizes the energy transfer area per unit fuel volume. In a baseline system dissociated hydrogen at 100 bar is heated to 6000 K, providing 2000 second of Isp. Fission fragments and intense radian field enhance the dissociation of molecular hydrogen beyond the equilibrium thermodynamic level. Uranium droplets in the core are confined and separated by an axisymmetric vortex flow generated by high velocity tangential injection of hydrogen in the mid-core regions. Droplet uranium flow to the core is controlled and adjusted by a twin flow nozzle injection system. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 91A52409
AIAA PAPER 91-3514 |
| 権利 | Copyright |
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