N. Sako et al., CanSat suborbital launch experiment - University educational space programusing can sized pico-satellite, ACT ASTRONA, 48(5-12), 2001, pp. 767-776
Our laboratory is proceeding with a project to design and fabricate a nano
satellite named "Gekkabijin" as "CanSat" project. This project was agreed a
t USSS'98 as a Japan-U.S. joint venture to make satellites for educational
purpose. CanSat is, as can be imaged from the name, a Coke can shaped and s
ized satellite. Our CanSat "Gekkabijin" was designed to deploy a thin flexi
ble membrane using centrifugal force. Before we can launch a CanSat into sp
ace, we had a chance to put it into sub-orbit with a support from a U.S. am
ateur rocket group in the name of ARLISS Project. ARLISS Project has alread
y taken place twice in 1999 and 2000 and we carried out 6 missions. This pa
per describes title objectives, satellite design, experiment results and le
ssons learned of University of Tokyo CanSat Project. (C) 2001 International
Astronautical Federation. Published by Elsevier Science Ltd.