airplane for such storage aside from the obvious advantage of enabling aircraft deployment of greater magnitude this feature of the invention will provide greater undetectable visibility and protection in such deployment fig5 a plan view of the configuration shown in fig4 illustrates how the leading edges of the wings 16 may be sculptured to accommodate the engine 18 if necessary in its vertical operating mode upon rotation a portion of the engine 18 may extend into the plane of the wing 16 depending upon the geometries involved and the position of the rotational axis 25 in order to eliminate interference between the engine 18 and the wind 16 a notch 27 is provided in the wing it should be understood that the mounting for the engine 18 if desired could be more than a simple pivot providing for translational as well as rotational motion of the engine 18 so that the engine 18 could be maintained below the wing level at all times thereby making the notch 27 unnecessary furthermore the engine 18 may be suspended from the wing 16 rather than being attached to the fuselage 13 in certain designs if suspended from the wings the pivot axis of the engines 18 would be operatively connected to that of the front section 13 and tail section 14 so as to be movable therewith a mechanism for opening or closing the fuselage is provided as shown by fig6 it.