| タイトル | Low energy trajectories to Mars via gravity assist from Venus to earth |
| 著者（英） | Williams, S. N.; Longuski, J. M. |
| 著者所属（英） | Purdue Univ.|Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1991-08-01 |
| 言語 | eng |
| 内容記述 | The analytical determination of launch dates and proposed trajectories is reviewed with respect to the search for a low-energy trajectory to Mars with gravitational assist from Venus for the years 1995-2024. Both Ballistic and Venus-Earth gravity assist (VEGA) trajectories are calculated with an automated design tool by the authors (1990). The trajectories are modeled as conic sections from one gravitating body to the next, and gravity assist is considered to act impulsively. VEGA trajectories to Mars require similar launch energies for 6 years listed and have moderate arrival C3s, with the lowest C3 requirement in 2015. The flight time and arrival energies of the trajectories are found to be larger than those of ballistic trajectories, but the low-energy launch window makes them desirable for unmanned Mars missions, in particular. |
| NASA分類 | ASTRODYNAMICS |
| レポートNO | 91A48850 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/346241 |
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