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Copyright Dr. Eng. Jan Pająk



Img.065 (G16) An overhead view of one cell of the flying system arranged from four stacked cigar-shaped complexes joined rim-to-rim by the forces of attraction from their side propulsors. In order to form such forces, outlets from propulsors marked with the same letters must face each other in neighbourly vehicles (e.g. the outlet of U propulsors in vehicles 4 must face the outlet of the U propulsors in vehicles 3). The diagram illustrates that the dimensions of the Magnocraft must obey the equation (G12) “D = d/√2” which stems from the Pythagoras Equation (see also Img.057 (G12), Img.087 (G37), and equation G34).
Symbols: M – main propulsors; U, V, W, X - four groups of side propulsors the output of which pulsates with mutual phase shifts of 90°; Z - central axis of the cell (the outer edge of each Magnocraft forming this single cell of the flying system must touch the Z axis); d - the nominal diameter of the circle on which centres of the side propulsors within each spacecraft are located; D - the outer diameter of the Magnocraft. Indexes 1 and 3 are attributed to the spacecraft oriented in the upright position, indexes 2 and 4 are assigned to the spacecraft in the inverted position.

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