| タイトル | Approach strategy for the rendezvous with comet Tempel 2 |
| 著者（英） | Kakuda, R. Y.; Dickey, L. E.; Ionasescu, R. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech.|Texas Univ. |
| 発行日 | 1986-01-01 |
| 言語 | eng |
| 内容記述 | The methods used to locate the comet nucleus and safety navigate through the debris surrounding the comet are discussed. The approach to the nucleus is in two parts: a high-speed (1.9 km/s) leg which ends with the spacecraft 200,000 km sunward of the nucleus, and a low-speed (25 m/s) leg which traverses the 200,000 km to the nucleus. The nucleus will be recovered by the narrow-angle camera 30 days prior to the completion of the high-speed inbound leg. The debris density is low enough to permit the safe passage of the spacecraft through the surrounding cometary debris. |
| NASA分類 | ASTRODYNAMICS |
| レポートNO | 86A47920
AIAA PAPER 86-2116 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/383085 |
