NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
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.

Related Records

IDRelationTitle19830016610Collected WorksThe 17th Aerospace Mechanisms Symposium
No Preview Available