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Basic space payload fastenerA new basic space fastener has been developed and tested by the GSFC. The purposes of this fastener are to permit assembly and servicing in space by astronauts and/or robots and to facilitate qualification of payloads on Earth prior to launch by saving time and money during the systems integration and component testing and qualification processes. The space fastener is a rework of the basic machine screw such that crossthreading is impossible; it is self-locking and will not work its way out during launch (vibration proof); it will not wear out despite repeated use; it occupies a small foot print which is comparable to its machine screw equivalent, and it provides force and exhibits strength comparable to its machine screw equivalent. Construction is ultra-simple and cost effective and the principle is applicable across the full range of screw sizes ranging from a #10 screw to 2.5 cm (1 in) or more. In this paper, the fastener principles of operation will be discussed along with test results and construction details. The new fastener also has considerable potential in the commercial sector. A few promising applications will be presented.
Document ID
19950020853
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vranish, J. M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Gorevan, Stephen
(Honeybee Robotics Ltd. New York, NY., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Publication Information
Publication: NASA. Johnson Space Center, The 29th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
95N27273
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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