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 :
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