Abstract: A vertical take-off and landing high speed aircraft comprising a fuselage having a first and a second end; a first pair of wings positioned between the first and second end; a secondary pair of wings positioned at the second end, wherein the first and second pairs of wings are joined by a pair of booms, each boom of the pair of booms having an fore end and an aft end; a drive propeller positioned at the first or second end; and a plurality of lift rotors positioned at the fore and aft ends of the pair of booms, the plurality of lift rotors providing a lift force necessary for vertical take-off and landing.