to the longitudinal axis of the wing whereby to rotate the wing member relative to the direction of flight the vehicle takes off and lands with the longitudinal wing axis being transverse to the direction of thrust and therefore to the flight direction in a manner similar to that of conventional aircraft in flight as the vehicle approaches space the rotating means rotates the longitudinal wing axis into alignment with the direction of thrust of the plurality of propulsion systems and therefore to the direction of flight for suborbital orbital and space flight in the manner similar to that of conventional rockets application_number US 74449185 A description the swing wing aerodynamic vehicle of the present invention is shown generally at 100 in fig1 the swing wing aerodynamic vehicle 100 comprises an elongated wing member 102 and a plurality of relatively rotatable propulsion systems 110 and 108 wing member 102 may include aerodynamic control surfaces 106 positioned about the forward and aft edges of the wing member 102 these aerodynamic control surface 106 would provide aerodynamic stability and control to the swing wing of this embodiment the propulsion system includes first motor 108 and second motor 110 plus respective rotation control devices 109 and 111 the first and second motors 108 and 110 are rotatably connected to the wing member at respective control rotation couplings 115 and 117 further the exhausts of the respective motors are controllable relative to the horizontal plane of the wing member by controllable exhaust gimbaling to control the attitude of the exhaust in the preferred embodiment the first and second motors 108 and 110 may be any combination of either conventional air breathing jet engines for low altitude aerodynamic flight or rocket motors using internal fuel.