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Miles M.52

WWII (1939–1945)

Miles M.52 — Fixed Wing
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The Miles M.52 was a turbojet-powered supersonic research aircraft project designed in the United Kingdom in the mid-1940s. In October 1943, Miles Aircraft was issued with a contract to produce the aircraft in accordance with Air Ministry Specification E.24/43. The programme was highly ambitious for its time, aiming to produce an aircraft capable of a speed of at least 1,000 miles per hour (1,600 km/h) during level flight, and involved a very high proportion of cutting-edge aerodynamic research and innovative design work.

Specifications

Category
Fixed Wing
Domain
Defence
Era
WWII (1939–1945)
Engine
1× turbojet engine with augmentor fan and afterburner
Thrust / Power
2000 lbf
Length (ft)
28
Wingspan (ft)
27
MTOW (lb)
7710