CanSat suborbital launch experiment - University educational space programusing can sized pico-satellite

Citation
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
Citations number
5
Categorie Soggetti
Aereospace Engineering
Journal title
ACTA ASTRONAUTICA
ISSN journal
00945765 → ACNP
Volume
48
Issue
5-12
Year of publication
2001
Pages
767 - 776
Database
ISI
SICI code
0094-5765(200103/06)48:5-12<767:CSLE-U>2.0.ZU;2-N
Abstract
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.