The Dassault 167 features a sleek and aerodynamic design, characterized by a slender fuselage, a delta wing configuration, and a distinctive tail section. The aircraft is powered by a single SNECMA Atar 9B turbojet engine, which provides a maximum thrust of approximately 6,000 kgf (58.8 kN). The Dass 167 has a maximum takeoff weight of around 9,200 kg (20,300 lb) and a top speed of over Mach 1.4 (1,450 km/h or 900 mph).
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By exploring the Dass 167 and its significance, we can gain a deeper understanding of the aviation industry and its evolution over the years. The Dass 167 link is a reminder of the innovative spirit and passion for aviation that drives us forward.
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The Dassault 167 was first introduced in the 1950s as a successor to the earlier Dassault 156, with the primary goal of creating a high-speed, multi-role fighter aircraft capable of performing various tasks, including air superiority, ground attack, and reconnaissance. The Dass 167 was designed to meet the requirements of the French Air Force (Armée de l'Air) and the French Navy (Marine nationale), which sought a highly maneuverable and versatile aircraft to replace their aging fleets.