Connection arrangement, aircraft or spacecraft, method for dropping load and method for landing
Abstract:
A connection arrangement having: a fuselage portion; a wing portion which is mounted on the fuselage portion in an upper region thereof; a first Z-coupling element which couples the wing portion to the fuselage portion in the vertical direction thereof; and two XZ-coupling elements which couple the wing portion to the fuselage portion in the vertical direction and longitudinal direction thereof; the first Z-coupling element being longitudinally adjustable in the vertical direction in order to thus adjust an angle of attack of the wing portion.
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