Journal of The Japan Society of Microgravity Application
Print ISSN : 0915-3616
Development of A Micro-gravity Experiment System Using A High Altitude Balloon
Tatsuaki HASHIMOTOShujiro SAWAIShin'ichiro SAKAINobutaka BANDOHiroaki KOBAYASHITakehiko ISHIKAWAYuko INATOMIKazuhisa FUJITATetsuo YOSHIMITSUYoshitaka SAITOHideyuki FUKE
Author information
JOURNAL OPEN ACCESS

2009 Volume 26 Issue 1 Pages 9-

Details
Abstract

To realize micro-gravity environment of long duration and good quality with moderate cost, an experimental system which is released from a high altitude balloon has developed. The system has a double-shell drag-free structure and the outer shell, namely flight capsule, is controlled not to collide with the inner shell to realize micro-gravity environment of good quality. This paper shows the design philosophy and the configuration of the system. The system was successfully tested twice, in May, 2006 and in May, 2007. Outline of the test results and future development plan are also described. Key Words: High-altitude balloon, Micro gravity, Drag-free, Supersonic.

Content from these authors
© 2009 The Japan Society of Microgravity Application
Previous article Next article
feedback
Top