Abstract: A split mirror vision augmentation system for high performance aircraft is disclosed comprising a transparency, an adjustable external mirror, a first internal mirror, and at least a second internal mirror. The external mirror is positionable at a stowed position adjacent to the transparency and substantially flush with the outer skin and is also positionable at at least one deployed position for reflecting light received from a field-of-view exterior to the aircraft. The first internal mirror is located within the aircraft, at an orientation substantially parallel to the external mirror. It receives a first portion of the light reflected from the external mirror and through the transparency. When the external mirror is deployed, the first internal mirror is constructed and arranged to redirect the reflected first portion of light toward a crew member of the aircraft. Thus, a first view is provided from the vantage of a first "apparent eye" position located aft of the external mirror.