Investigating the Interaction Between Reconfigurability and System Mass Using Multidisciplinary Design Optimization

Author:

Ferguson Scott,Lewis Kemper

Publisher

American Institute of Aeronautics and Astronautics

Reference30 articles.

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2. 2Peterson, L. D., and Agnes, G. S. "How the Mass of Large Gossamer OpticalTelescopes Scales with Size and Disturbance Environment,"48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Honolulu, HI, 2007, AIAA Paper AIAA-2007-1813.

3. 3Gordon, G. D. "Space Exploration: Mass Ratios for Different Missions," AIAA Space 2007 Conference and Exposition, Long Beach, CA, 2007, AIAA Paper AIAA-2007-6278.

4. 4Bayley,D.J.,Hartfield,R.J.,Burkhalter,J.E.,andJenkins,R.M."DesignOptimizationofaSpaceLaunchVehicleUsing a Genetic Algorithm," 3rdAIAA Multidisciplinary Design Optimization Specialist Conference, Honolulu, HI, 2007, AIAA Paper AIAA-2007-1863.

5. 5Kim,D.J.,Wilson,J.,Chiang,J.,andHom,S."SS/LHistoricalTrendsonSatelliteMassGrowth,"25thAIAAInternational Communications Satellite Systems Conference, Seoul, SouthKorea, 2007, AIAA Paper AIAA-2007-3220.

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