MODAL TEST OF A LARGE SPACECRAFT USING A MASS-LOADED INTERFACE

A finite-element mathematical model of a large spacecraft structure is validated through a modal test survey. The spacecraft is bolted via its adapter to a steel base plate which served as an inertial reaction mass. The inertial base plate supported by five low-frequency air supports provides a free...

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Veröffentlicht in:	Experimental techniques (Westport, Conn.) Conn.), 1992-11, Vol.16 (6), p.15-20
Hauptverfasser:	Haughton, J.M., Hauser, J.A., Turner, L.M.
Format:	Artikel
Sprache:	eng
Online-Zugang:	Volltext
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