Vaccum Deployment and Testing of a 20M Solar Sail System
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American Institute of Aeronautics and Astronautics
Reference13 articles.
1. Sleight, D., Mann, T., Lichodziejewski, D., Derbès, B. "Structural Analysis and Test Comparison of a 20m Inflation Controlled Solar Sail", 47thAIAA/ASME/ASCE/AHS/ASC/GSF Structural Dynamics & Materials Conference, Newport RI,AIAA-2006-1706, May1-4, 2006
2. Mann, T. Behun, V., Lichodziejewski, D. Derbes, B. Sleight, D. "Ground Testing a 20m inflation Deployed Solar Sail", 47thAIAA/ASME/ASCE/AHS/ASC/GSF Structural Dynamics &Materials Conference, Newport RI, AIAA-2006-1707, May1-4, 2006
3. Lichodziejewski, D., Derbes, B., Friese, D., Galeana, D. "Vacuum Deployment of a 4-Quadrant Scalable Inflatable Rigidizable Solar Sail System", 40thAIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tuscon, AZ,AIAA-2005-3927, July11-13, 2005
4. Sleight, D. W., Michii, Y., Mann T., Slade, K., Wang, J., Lichodziejewski, D., Derbès B. "Finite Element Analysis and Test Correlation of a 10-Meter Inflation Deployed Solar Sail".46thAIAA/ASME/ASCE/AHS/ASC/GSF Structures, Structural Dynamics & Materials Conference, Austin, TX, AIAA-2005-2121,Apr 18-21, 2005.
5. Lichodziejewski, D., Derbès, B., Reinert, R., Bevin, K., Slade, K., and Mann, T. "Development and Ground Testing of a Compactly Stowed Scalable Inflatably Deployed Solar Sail,"45thAIAA/ASME/ASCE/AHS/ASC/GSF Structures, Structural Dynamics &Materials Conference, PalmSprings, CA, AIAA-2004-1507, 2004.
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