| タイトル | Mars transportation system |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940021196 |
| 著者（英） | Garrard, William; Rutherford, Dave; Vano, Andrew |
| 著者所属（英） | Minnesota Univ. |
| 発行日 | 1992-01-01 |
| 言語 | eng |
| 内容記述 | The University of Minnesota Advanced Space Design Program has developed a sample Mars exploration scenario. The purpose of the design project is to enhance NASA and university interaction, to provide fresh ideas to NASA, and to provide real world design problems to engineering students. The Mars Transportation System in this paper is designed to transport a crew of six astronauts to the Martian surface and return them to Low Earth Orbit (LEO) starting in the year 2016. The proposed vehicle features such advanced technologies as nuclear propulsion, nuclear power generation, and aerobraking. Three missions are planned. Orbital trajectories are of the conjunction class with an inbound Venus swingby providing a 60-day surface stay at Mars and an average total trip time of 520 days. |
| NASA分類 | MECHANICAL ENGINEERING |
| レポートNO | 94N25689 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/113359 |
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