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Deployment hinge using wraparound stripsAerospatiale developed a new appendage deployment concept called AMEDE (French acronym for improvement of deployment mechanisms) with a view toward increased simplicity and functional reliability. This new concept, applicable to the deployment of any type of spaceborne appendage (in particular to solar arrays), enables deployment without synchronization or speed regulation devices. On the other hand, it requires the use of hinges with low driving or resistive torques. The AMEDE concept is compared with the conventional deployment concept. The conceptual and functional principles for the ADELE hinge are presented, as well as the hinges' main characteristics. The development status of both the AMEDE concept and the ADELE (French acronym for deployment hinge using wraparound strips) hinge are addressed.
Document ID
19920015827
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blanc, Eric
(Aerospatiale Cannes, France)
Date Acquired
September 6, 2013
Publication Date
May 1, 1992
Publication Information
Publication: NASA. Goddard Space Flight Center, The 26th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
92N25070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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