| タイトル | Nanosail-D: The Small Satellite That Could! |
| 本文（外部サイト） | http://hdl.handle.net/2060/20110015650 |
| 著者（英） | Agasid, Elwood F.; Kitts, Christopher; Casas, Joseph P.; O'Brien, Sue; Adams, Charles L.; Laue, Greg; Alhorn, Dean C. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2011-08-08 |
| 言語 | eng |
| 内容記述 | Three years from its initial design review, NanoSail-D successfully deployed its sail on January 20th, 2011. It became the first solar sail vehicle to orbit the earth and the second sail ever unfurled in space. The NanoSail-D mission had two main objectives: eject a nanosatellite from a microsatellite; deploy its sail from a highly compacted volume and low mass system to validate large structure deployment and potential de-orbit technologies. These objectives were successfully achieved and the de-orbit analysis is in process. This paper presents an overview of the NanoSail-D project and insights into how potential setbacks were overcome. Many lessons have been learned during these past three years and are discussed in light of the phenomenal success and interest that this small satellite has generated. NanoSail-D was jointly designed and built by NASA's Marshall Space Flight Center and NASA's Ames Research Center. ManTech/NeXolve Corporation also provided key sail design support. The NanoSail-D experiment is managed by Marshall and jointly sponsored by the Army Space and Missile Defense Command, the Von Braun Center for Science and Innovation and Dynetics Inc. Ground operations support was provided by Santa Clara University, with radio beacon packets received from amateur operators around the world. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | M11-0547
SSC11-V-1
M11-0294
M11-0861 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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