The HA-300 was an Egyptian single-seater lightweight fighter aircraft first flown in 1964 and developed from the abortive Spanish Hispano HA-300 delta-wing fighter, work on the development of which was carried out in the late 1950's. The HA-300 was a mid-wing cantilever monoplane of delta platform powered by a Bristol Siddeley Orpheus Bor.2 turbojet engine providing a design speed of Mach 2.2. Research HA-300
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Abbreviations
Research HA-300
