Lessons learned from small space systems development using magnesium alloys

Materials Science Forum

Volumn 419-422, Issue I, 2003, Pages 219-224

  Matunaga, Saburo ^a   Sawada, Hirotaka ^a   Furuya, Hiroshi ^a   Kogiso, Nozomu ^b  

^a TOKYO INSTITUTE OF TECHNOLOGY   (Japan)

^b Osaka Prefecture University   (Japan)

Author keywords

Cansat; Cubesat; Docking mechanism; Magnesium alloys; Small space systems

Indexed keywords

CAMERAS; CHARGE COUPLED DEVICES; DOCKING; ORBITS; SATELLITES; SPACE APPLICATIONS; SURFACE TREATMENT;

SPACE SYSTEMS;

MAGNESIUM ALLOYS;

EID: 0037246253     PISSN: 02555476     EISSN: 16629752     Source Type: Book Series    
DOI: 10.4028/www.scientific.net/msf.419-422.219     Document Type: Conference Paper

References (4)

1. Koji Nakaya, Shingo Tsurumi, Hirotaka Sawada, Makoto Mori, Kyoichi Ui, Ruichi Hodoshima, Naohide Maeda, Hideto Okada, Naoki Miyashita, Masafumi Iai, Kazuya Konoue, Osamu Mori and Saburo Matunaga, "Titech CanSat Project 2000: Sub-Orbital Flight and Balloon Experiment," the Journal of Space Technology and Science, Vol. 16, No. 1, 2000, pp.9-18.
2. Kyoichi Ui, Koji Nakaya, Hirotaka Sawada, Naoki Miyashita, Masafumi Iai, Saburo Matunaga, "Small Docking Mechanism with Grasping and Guiding Function for Small Mothership-Daughtership Satellite," 23rd International Symposium on Space Technology and Science (ISTS), Matsue, Shimane, May 27-June 1, 2002-d-05, 2002.
3. Hirotaka SAWADA, Kazuya KONOUE, Koji NAKAYA, Kyoichi UI, Ryuichi HODOSHIMA, Naohide MAEDA, Hideto OKADA, Naoki MIYASHITA, Masafumi IAI and Saburo MATUNAGA, "TITech CubeSat Project and Development of CUTE-I," 23rd International Symposium on Space Technology and Science (ISTS), Matsue, Shimane, May 27-June 1, 2002-f-11, 2002.
4. URL of Tokyo Institute of Technology: http://horse.mes.titech.ac.jp/srtlssp/index.html