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Deployment and release mechanisms on the Swedish satellite, VIKINGTwo mechanism types are presented, a rigid boom system and a 'hold and release' mechanism for spherical sensors. Both mechanisms have been designed, developed and tested by Saab-Space AB, Linkoping, Sweden for the VIKING project under a contract from the Swedish Space Corporation.
Document ID
19830016630
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Eriksson, S. (Saab-Space A.B. Linkoeping, Sweden)
Date Acquired
August 11, 2013
Publication Date
May 1, 1983
Publication Information
Publication: JPL The 17th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
83N24901
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19830016610Collected WorksThe 17th Aerospace Mechanisms Symposium19830016610Collected WorksThe 17th Aerospace Mechanisms Symposium
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