Computer Science
Scientific paper
Jul 2005
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005esasp.591..171a&link_type=abstract
In: Proceedings of the 11th European Space Mechanisms and Tribology Symposium, ESMATS 2005, 21-23 September 2005, Lucerne, Switz
Computer Science
Deployment And Hold-Down Mechanisms
Scientific paper
A single-point-actuated, multi degree-of-freedom restraining launch latch mechanism was developed for a two-degree of freedom tilt table antenna gimbal. The design of the launch latch protects the gimbal pivots and actuators through launch vibration, and precludes any high forces on sensitive gimbal components as a result of operation of the latch mechanism itself. At the same time, stringent requirements on stiffness for the latched gimbal and payload are met. The launch latch design was carried through to qualification largely as initially conceived; however, detail design changes and improvements were made during development as a result of prototyping and development testing.
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