Optimum Power Plant Configuration for a Supersonic V/S.T.O.L Strike Aircraft

Abstract

Examples of jet‐lift aircraft powered by the diverse systems of the single lift/thrust turbofan and the multi‐engined specialized lifting and propulsion engines are now flying. With the experience gained from these pioneering aircraft, it is appropriate to review the thermodynamic characteristics required of engines for future ‘vectored thrust’ low‐level strike aircraft, having supersonic capability. The relative merits of extreme forms of power plant are discussed from the engine and power plant designer's viewpoint and these are linked with a spectrum of aircraft which lie between these extremes of design.