The proceedings of the JSME annual meeting
Online ISSN : 2433-1325
2006.5
Session ID : 1012
Conference information
1012 System Design and In-flight Evaluation of Microgravity Experimental Device using High-altitude Balloon
Kenichi TAJIMAShujiro SAWAIShinichiro SAKAINobutaka BANDOTatsuaki HASHIMOTOShinji HOSHINO
Author information
CONFERENCE PROCEEDINGS RESTRICTED ACCESS

Details
Abstract

Balloon-based Operation Vehicle (BOV) is currently developed at JAXA for the realization of microgravity environment. As for this research, second experiment of 2006 and third experiment of 2007 are already planned. As a member of the control and electric system group, we estimate a method to detect the relative position of an integumentary covering as an inner shell of an experimental device with laser sensors. In this paper is explained a summary of a microgravity experimental device and shown it about an experiment performed in May, 2006.

Content from these authors
© 2006 The Japan Society of Mechanical Engineers
Previous article Next article
feedback
Top