The Bell D-188A was a proposed eight-engine, Mach 2 capable vertical take-off and landing tiltjet fighter that never proceeded past the mock-up stage. In 1955 the USAF and the US Navy both asked Bell Aircraft to develop a supersonic all-weather fighter-bomber and interceptor, designated the Model 2000 and offered as the D-188 for the Navy and the D-188A for the Air Force. Four General Electric J85 engines sat in wing pods that rotated to direct thrust downward for takeoff, and four more engines were in the fuselage, two of them vertical liftjets. Bell showed the design publicly on 5 December 1960 as the XF-109, although that designation was never officially assigned, and in spring 1961 the Air Force cancelled the program with no aircraft built.
Facts
Engine Class StatusDesign only (never built) 1 EngineEight General Electric J85-GE-5 turbojets 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Of Make
Source Bell D-188A (Wikipedia)
Sources
1. Bell D-188A (Wikipedia)
Lead, public showing
On 5 December 1960, Bell publicly showed off the design as the XF-109
Specifications, empty weight
Empty weight: 13,800 lb (6,260 kg)
Specifications, powerplant
Powerplant: 8 × General Electric J85-GE-5 turbojets, 2,600 lbf (12 kN) thrust each
Lead, aircraft description
The Bell D-188A (unofficial military designations XF-109/XF3L) was a proposed eight-engine Mach 2
Lead, design status
never proceeded past the mock-up stage
Lead, builder
In 1955, Bell Aircraft was requested by both the USAF and the US Navy to develop a VTOL/STOVL supersonic, all-weather fighter-bomber and defence interceptor.
In Group: Jet Fighters and Interceptors, Lead, role of the aircraft
The Bell D-188A (unofficial military designations XF-109/XF3L) was a proposed eight-engine Mach 2-capable vertical take-off and landing (VTOL) tiltjet fighter that never proceeded past the mock-up stage.
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