| タイトル | Finding Acceptable James Webb Space Telescope Mission Orbits From a Fixed Ariane Flight Profile |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050210121 |
| 著者（英） | Janes, Leigh; Beckman, Mark |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 2005-01-01 |
| 言語 | eng |
| 内容記述 | The James Webb Space Telescope (JWST) will be launched into orbit about the Sun/Earth L2 libration point. Trajectory design was recently completed which included expected separation states from the Ariane launch vehicle, constraints such as eclipses, maximum orbit size, maximum Sun-Vehicle-Earth/Moon angles, and launch opportunities. The results of this trajectory design give a set of possible trajectories for JWST with bounded stray light zones and provide a complete launch window. This data is also used to design the initial trajectory correction maneuver such that a maneuver towards the Sun is not required. |
| NASA分類 | Space Sciences (General) |
| レポートNO | AAS-05-271 |
| 権利 | No Copyright |
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