| タイトル | Trajectory Design from GTO to Near-Equatorial Lunar Orbit for the Dark Ages Radio Explorer (DARE) Spacecraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/20150022372 |
| 著者（英） | Galal, Ken F.; Landin, Brett; Mitchell, Scott; Genova, Anthony L.; Yang Yang, Fan; Perez, Andres Dono; Faber, Nicolas T.; Burns, Jack O. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2015-01-01 |
| 言語 | eng |
| 内容記述 | The trajectory design for the Dark Ages Radio Explorer (DARE) mission concept involves launching the DARE spacecraft into a geosynchronous transfer orbit (GTO) as a secondary payload. From GTO, the spacecraft then transfers to a lunar orbit that is stable (i.e., no station-keeping maneuvers are required with minimum perilune altitude always above 40 km) and allows for more than 1,000 cumulative hours for science measurements in the radio-quiet region located on the lunar farside. |
| NASA分類 | Engineering (General) |
| レポートNO | AAS-15-456
ARC-E-DAA-TN21205 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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