| タイトル | Large inclination change using lunar-swingby techniques |
| 著者（英） | Hsu, S.; Roberts, C. E.; Dunham, D. W.; Lee, T.; Engel, C. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1988-01-01 |
| 言語 | eng |
| 内容記述 | The use of lunar-swingby maneuvers to transfer a spacecraft from an equatorial orbit to a polar orbit has been investigated in order to verify the technical feasibility of the NASA/ESA equatorial science phase (ESP)/Cluster mission. The solar aspect angle constraints of the spacecraft spin-axis and the dependence of the total Delta-V cost of the transfer on the initial ESP orbital parameters (particularly perigee radius and inclination) have been studied. The results indicate that a satisfactory ESP-to-Cluster orbit transfer can be achieved using a double lunar-swingby sequence. |
| NASA分類 | ASTRODYNAMICS |
| レポートNO | 88A50417
AIAA PAPER 88-4290 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/369108 |
