| タイトル | Designing Phase 2 for the Double-Lunar Swingby of the Magnetospheric Multiscale Mission (MMS) |
| 本文（外部サイト） | http://hdl.handle.net/2060/20030025708 |
| 著者（英） | Edery, Ariel |
| 著者所属（英） | AI Solutions, Inc. |
| 発行日 | 2002-01-01 |
| 言語 | eng |
| 内容記述 | The Magnetospheric Multiscale (MMS) mission is a formation flying mission that consists of four distinct phases: phases 1 and 2 are low-inclination highly elliptical orbits (HEO), phase 3 is a double-lunar swingby which transfers phase 2 to phase 4, a high-inclination HE0 orbit. Phase 2 is designed to reach the first lunar swingby of phase 3 in the most efficient fashion. It is shown that when the orientation of the line of apsides of phase 2 is properly chosen, no extra Delta-V is required beyond what is typically needed to raise apogee to lunar distance. |
| NASA分類 | Spacecraft Instrumentation and Astrionics |
| 権利 | No Copyright |
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