Continuum structural representation of flexure and tension stiffened one-dimensional spacecraft architectures
Spacecraft designs are a result of system properties and design variables that ensure the spacecraft will operate to mission objectives. The focus of this effort is a set of global system variables for frequency, length, total mass and the ratio between the payload mass and the support structure mas...
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| Language: | en |
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2009
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| Online Access: | http://etd.lib.montana.edu/etd/2009/larsen/LarsenJ0809.pdf |