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Evolution from a hinge actuator mechanism to an antenna deployment mechanism for use on the European large communications satellite (L-SAT/OLYMPUS)The evolution of an Antenna Deployment Mechanism (ADM) from a Hinge Actuator Mechanism (HAM) is described as it pertains to the deployment of large satellite antennas. Design analysis and mechanical tests are examined in detail.
Document ID
19840017016
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Death, M. D. (British Aerospace Dynamics Group Stevenage, United Kingdom)
Date Acquired
August 12, 2013
Publication Date
May 1, 1984
Publication Information
Publication: NASA. Goddard Space Flight Center The 18th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
84N25084
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19840017010Collected WorksThe 18th Aerospace Mechanisms Symposium
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