Microgravity vibration isolation for the International Space Station

被引:0
|
作者
Whorton, MS [1 ]
机构
[1] NASA, George C Marshall Space Flight Ctr, TD55 Vehicle Control Syst, Huntsville, AL 35812 USA
来源
SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM, PTS 1 AND 2 | 2000年 / 504卷
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D O I
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中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The International Space Station (ISS) is being envisioned as a laboratory for experiments in numerous microgravity (mu g) science disciplines. Predictions of the ISS acceleration environment indicate that the ambient acceleration levels will exceed levels that can be tolerated by the science experiments. Hence, microgravity vibration isolation systems are being developed to attenuate the accelerations to acceptable levels. While passive isolation systems are beneficial in certain applications, active isolation systems are required to provide attenuation at low frequencies and to mitigate directly induced payload disturbances. To date, three active isolation systems have been successfully tested in the orbital environment. A fourth system called g-LIMIT is currently being developed for the Microgravity Science Glovebox and is manifested for launch on the UF-1 mission. This paper presents an overview of microgravity vibration isolation technology and the g-LIMIT system in particular.
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收藏
页码:605 / 610
页数:6
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