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Fluid Quick Disconnects - ISS Lessons LearnedThe International Space Station has many fluid systems on the United States On-orbit Segment supporting thermal control, life support, extravehicular activities and payloads. To facilitate assembly and maintenance, fluid quick disconnect (QD) fittings are used throughout these systems for both internal pressurized modules and for external systems exposed to space. In the years since full scale development began on these QDs, a number of design and performance issues have surfaced and required substantial program funds and activity to rectify. This paper is intended to describe the most significant of these issues, their resolutions, and the lessons learned from the ISS experience.
Document ID
20080026345
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Bond, Timothy A.
(NASA Johnson Space Center Houston, TX, United States)
Morrison, Russell H.
(Boeing Co. Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
July 17, 2006
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Norfolk, VA
Country: United States
Start Date: July 17, 2006
End Date: July 20, 2006
Sponsors: Society of Automotive Engineers, Inc.
Funding Number(s)
OTHER: 401769
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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