| タイトル | Low Pressure Nuclear Thermal Rocket (LPNTR) concept |
| 本文（外部サイト） | http://hdl.handle.net/2060/19920001876 |
| 著者（英） | Ramsthaler, J. H. |
| 著者所属（英） | Idaho National Engineering Lab. |
| 発行日 | 1991-01-01 |
| 言語 | eng |
| 内容記述 | A background and a description of the low pressure nuclear thermal system are presented. Performance, mission analysis, development, critical issues, and some conclusions are discussed. The following subject areas are covered: LPNTR's inherent advantages in critical NTR requirement; reactor trade studies; reference LPNTR; internal configuration and flow of preliminary LPNTR; particle bed fuel assembly; preliminary LPNTR neutronic study results; multiple LPNTR engine concept; tank and engine configuration for mission analysis; LPNTR reliability potential; LPNTR development program; and LPNTR program costs. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 92N11094 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/130245 |
