| Autor: |
James C. Goodding, Lawrence M. Robertson, D. T. Griffith, Ingram, Brea R. (Us Air Force Research Lab, Kirtland Afb, Nm), Vit Babuska |
| Rok vydání: |
2007 |
| Předmět: |
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| Zdroj: |
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. |
| DOI: |
10.2514/6.2007-2390 |
| Popis: |
Signal and power harnesses on spacecraft buses and payloads can alter structural dynamics, as has been noted in previous flight programs. The community, however, has never undertaken a thorough study to understand the impact of harness dynamics on spacecraft structures. The Air Force Research Laboratory is leading a test and analysis program to develop fundamental knowledge of how spacecraft harnesses impact dynamics and develop tools that structural designers could use to achieve accurate predictions of cable-dressed structures. The work described in this paper involved a beam under simulated free boundary conditions that served as a validation test bed for model development. |
| Databáze: |
OpenAIRE |
| Externí odkaz: |
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