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  • g of the present embodiment, is especially preferred [0128] With reference to FIG. 11C, in a variation of the seventh, preferred embodiment, two power pods 751 are located far out at the ends of the laterally extending tetrahedron element 723, making the aircraft into a span-loaded, swept flying wing. [0129] A Further Variation of the Embodiments [0130] The above described embodiments can each be
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