Tokyo Institute of Technology Graduate School of Science and Engineering
Tokyo Institute of Technology Graduate School of Science and Engineering
Tokyo Institute of Technology Graduate School of Science and Engineering
Tokyo Institute of Technology Graduate School of Science and Engineering
Tokyo Institute of Technology Graduate School of Science and Engineering
Tokyo Institute of Technology Interdisciplinary Graduate School of Science and Engineering
Tokyo Institute of Technology Graduate School of Science and Engineering
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
雑誌名
平成15年度アストロダイナミクスシンポジウム:講演後刷り集
雑誌名(英)
ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers
A separation system was developed for pico-satellite that had realized reliable separation without using pyrotechnic devices. This paper mainly describes results of vibration tests and separation tests under microgravity environment to evaluate the system's performance. In addition, this separation system was used for the launch of Cubesat on 30 June 2003 in Russia. So the results of launch are also described.
Development of pico-satellite separation system and launch results
