| タイトル | Propulsion System and Orbit Maneuver Integration in CubeSats: Trajectory Control Strategies Using Micro Ion Propulsion |
| 本文（外部サイト） | http://hdl.handle.net/2060/20150016067 |
| 著者（英） | Hudson, Jennifer; Martinez, Andres; Petro, Andrew |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2015-08-08 |
| 言語 | eng |
| 内容記述 | The Propulsion System and Orbit Maneuver Integration in CubeSats project aims to solve the challenges of integrating a micro electric propulsion system on a CubeSat in order to perform orbital maneuvers and control attitude. This represents a fundamentally new capability for CubeSats, which typically do not contain propulsion systems and cannot maneuver far beyond their initial orbits. |
| NASA分類 | Spacecraft Propulsion and Power; Astrodynamics |
| レポートNO | NASA FS-2015-03-30-ARC
ARC-E-DAA-TN25939 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
