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Innovative Escapement-Based Mechanism for Micro-Antenna Boom DeploymentThis paper presents the prototype of a tubular boom antenna developed for the Polish BRITE-PL satellite by the Space Research Center of the Polish Academy of Sciences (CBK PAN). What is unique about our work is that we developed an original type of the tubular boom antenna deployment mechanism that can be used widely as a basic solution for compact electrical antennas, booms deploying sensitive instruments, ultra-light planetary manipulators etc. The invented electromagnetic driving unit provides a dual complementary action - it adds extra energy to the driving spring, making the system more reliable, and at the same time it moderates the deployment speed acting as a kind of damper. That distinguishing feature predetermines the mechanism to be applied wherever the dynamic nature of a spring drive introducing dangerous vibrations and inducing severe local stress in the structure needs to be mitigated. Moreover, the paper reveals a product unique in Europe - a miniature beryllium bronze tubular boom free of geometry and strain defects, which is essential for stiffness and fatigue resistance. Both the deployment mechanism and the technology of tubular boom manufacturing are protected by patent rights.
Document ID
20150004084
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Tokarz, Marta
(Polish Academy of Sciences Warsaw, Poland)
Grygorczuk, Jerzy
(Polish Academy of Sciences Warsaw, Poland)
Jarzynka, Stanislaw
(Polish Academy of Sciences Warsaw, Poland)
Gut, Henryk
(GUTRONIC Warsaw)
Date Acquired
April 2, 2015
Publication Date
May 1, 2014
Publication Information
Publication: The 42nd Aerospace Mechanism Symposium
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Public Use Permitted.
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