| タイトル | Low-Enriched Uranium Nuclear Thermal Propulsion Systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/20170001462 |
| 著者（英） | Mitchell, Doyce P.; Houts, Michael G.; Aschenbrenner, Ken |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2017-02-02 |
| 言語 | eng |
| 内容記述 | The fundamental capability of Nuclear Thermal Propulsion (NTP) is game changing for space exploration. For example, using NTP for human Mars missions can provide faster transit and/or round trip times for crew; larger mission payloads; off nominal mission opportunities (including wider injection windows); and crew mission abort options not available from other architectures. The use of NTP can also reduce required earth-to-orbit launches, reducing cost and improving ground logistics. In addition to enabling robust human Mars mission architectures, NTP can be used on exploration missions throughout the solar system. A first generation NTP system could provide high thrust at a specific impulse above 900 s, roughly double that of state of the art chemical engines. Characteristics of fission and NTP indicate that useful first generation systems will provide a foundation for future systems with extremely high performance. Progress made under the NTP project could also help enable high performance fission power systems and Nuclear Electric Propulsion (NEP). Guidance, navigation, and control of NTP may have some unique but manageable characteristics. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | AAS Paper 17-144
MSFC-E-DAA-TN38873 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
