AIAA-2004-1796 Hybrid Interface Modal Model Formulation for Launch Vehicle Coupled Loads Analysis
45TH, Structures, structural dynamics, and materials conference:; 45th AIAA/ASME/ASCE/AHS/ASC 12th AIAA/ASME/AHS adaptive structures conference: 6th AIAA non-deterministic approaches forum: 5th AIAA gossamer spacecraft forum ; 2004 ; Palm Springs, Calif
2004-01-01
11 pages
Held in conjunction with 12th AIAA/ASME/AHS adaptive structures conference, 6th AIAA non-deterministic approaches forum and 5th AIAA gossamer spacecraft forum
Conference paper
English
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