|
A fractionated spacecraft is a satellite architecture where the functional capabilities of a conventional monolithic spacecraft are distributed across multiple modules which interact through wireless links. Unlike other aggregations of spacecraft, such as constellations and clusters, the modules of a fractionated spacecraft are largely heterogeneous and perform distinct functions corresponding, for instance, to the various subsystem elements of a traditional satellite. == History == The term "fractionated spacecraft" appears to have been coined by Owen Brown and Paul Eremenko in a series of 2006 papers,〔 〕〔 〕〔 〕 which argue that a fractionated architecture offers more flexibility and robustness than traditional satellite design during mission operations, and during the design and procurement. The idea dates back to at least a 1984 article by P. Molette.〔 〕 Molette's, and later analyses by Rooney, concluded that the benefits of fractionated spacecraft were outweighed by their higher mass and cost. By 2006, Brown and his collaborators〔〔 〕 claim that the option value of flexibility, the insurance value of improved robustness, and mass production effects will exceed any penalties, and make an analogy with distributed clusters of personal computers (PCs) which are overtaking supercomputers. A 2006 study by the Massachusetts Institute of Technology appears to have corroborated this latter view.〔 〕 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Fractionated spacecraft」の詳細全文を読む スポンサード リンク
|