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Northrop X-4 Bantam
'
Description
RoleExperimental semi-tailless
Crew1
First Flight December 16, 1948
ManufacturerNorthrop Corporation
Dimensions
Length22 ft 3 in7.1 m
Wingspan26 ft 10 in8.2 m
Height14 ft 10 in4.5 m
Wing areaft²
Weights
Empty5,600 lb2,540 kg
Loadedlbkg
Maximum takeoff7,820 lb3,550 kg
Powerplant
Engines2x Westinghouse J30 turbojets
Thrust (each)1,600 lb7.1 kN
Performance
Maximum speed640 mph1,035 km/h
Rangemileskm
Service ceiling44,000 ft13,400 m
Rate of climbft/minm/min
Wing loadinglb/ft²kg/m²
Thrust/Weight
Three view diagram
Northrop X-4 Bantam


The Northrop X-4 Bantam was a small twin-jet airplane that had no horizontal tail surfaces, depending instead on combined elevator and aileron control surfaces (called elevons) for control in pitch and roll attitudes. The hope of some aerodynamicists was that eliminating the horizontal tail would also do away with stability problems at transonic speeds resulting from the interaction of supersonic

shock waves from the wings and the horizontal stabilizers.

Two X-4s were built by the Northrop Corporation, but the first was found to be mechanically unsound and after 10 flights it was grounded and used to provide parts for the second.

While being tested from 1950 to 1953 at the NACA High-Speed Flight Research Station (now Edwards Air Force Base), the X-4's semi-tailless configuration exhibited inherent longitudinal stability problems (porpoising) as it approached the speed of sound. It was concluded that (with the control technology available at the time) tailless craft were not suited for transonic flight.

The surviving X-4 is on display at the USAF Museum.

1 Aircraft serial numbers

1 Also See

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