EXTENDED STUDY system and subsystem responses due to the dynamic OF THE VIBROACOUSTIC BEHAVIOUR interaction of the spacecraft structure and the sound field in the payload compartment. OF THE ARTEMIS ANTENNA REFLECTOR The frequency range 20-500 Hz is...
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EXTENDED STUDY system and subsystem responses due to the dynamic OF THE VIBROACOUSTIC BEHAVIOUR interaction of the spacecraft structure and the sound field in the payload compartment. OF THE ARTEMIS ANTENNA REFLECTOR The frequency range 20-500 Hz is particularly critical in Authors: D. VAUCHER de la CROIX1, J. CADIEUX1, terms of stresses and interface forces for sensitive C. THIRARD1,A. CALVI2, P. GUY3 structural components, such as antenna reflectors. 1 Critical loads can arise in the dish itself (e.g. in the face- METRAVIB RDS, 200 chemin des Ormeaux, sheets of the sandwich), in the connection between the F-69760 Limonest – France dish and its backing structure (e.g. cleats) or other Phone: 33 4 78 66 34 00 Fax: 33 4 78 66 34 34 e-mail : daniel.vaucherdelacroix@metravib.fr highly loaded areas of the antenna reflector. In other 2 ESA/ESTEC – TOS/MMS, Newtonweg 1 situations (large solar array panels in their stowed 2200-AG Noordwijk – The Netherlands position in launch configuration) h
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