DocumentCode
2491912
Title
Development of a fly-back CANSAT in 3 weeks
Author
Ümit, Mehmet Ertan ; Tetlow, Matthew ; Cabañas, Willy ; Akiyama, Hiroaki ; Yamaura, Shusaku ; Olaleye, Salu
Author_Institution
Space Syst. Design & Testing Lab., ITU Fac. of Aeronaut. & Astronaut., Istanbul, Turkey
fYear
2011
fDate
9-11 June 2011
Firstpage
804
Lastpage
807
Abstract
Two CanSats are developed in Wakayama University by international researchers in one month. The first CanSat was developed in less than three days. The second CanSat was more advanced and developed in three weeks. The design and development phases are explained in this paper.
Keywords
aerospace engineering; engineering education; space vehicle electronics; fly-back CANSAT; Educational institutions; Global Positioning System; Magnetometers; Magnetosphere; Microcontrollers; Testing; CanSat; Flight Control; Guidance; Navigation;
fLanguage
English
Publisher
ieee
Conference_Titel
Recent Advances in Space Technologies (RAST), 2011 5th International Conference on
Conference_Location
Istanbul
Print_ISBN
978-1-4244-9617-4
Type
conf
DOI
10.1109/RAST.2011.5966953
Filename
5966953
Link To Document