| タイトル | Neutronics analysis of an open-cycle high-impulse gas core reactor concept |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720013996 |
| 著者（英） | Whitmarsh, C. L., Jr. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1972-04-01 |
| 言語 | eng |
| 内容記述 | A procedure was developed to calculate the critical fuel mass, including the effects of propellant pressure, for coaxial-flow gas-core reactors operating at 196,600 newtons thrust and 4400 seconds specific impulse. Data were generated for a range of cavity diameter, reflector-moderator thickness, and quantity of structural material. Also presented are such core characteristics as upper limits on cavity pressure, spectral hardening in very-high-temperature hydrogen, and reactivity coefficients. |
| NASA分類 | NUCLEAR ENGINEERING |
| レポートNO | 72N21646
NASA-TM-X-2534
E-6390 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/203705 |
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