1988 | OriginalPaper | Buchkapitel
On Shape Optimization of Satelite Tanks
verfasst von : H. A. Eschenauer
Erschienen in: Structural Optimization
Verlag: Springer Netherlands
Enthalten in: Professional Book Archive
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In order to reduce the transportation cost incurred when sending a satellite into orbit, the weight of the satellite should be as low as possible. Even small reductions in the weight of the individual components lead to a decrease in the costs. One of these components is the satellite fuel tank, which stores the fuel required for positioning purposes for the entire lifetime of the satellite.