Length
18.9 m
Flat Wing Span
7.24 m
Height
3.89 m
Flat Wing Area
18.02 m²
Max Mach
2.3 Mach
Max Ceiling
18000 m
Number of Engines
8
Aircraft Engine
Number Built
1
Maximum Range
3900 km

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Aircraft Weight Variants

Aircraft Maximum Range (km)
Bell D-188A 3900
All data (20 fields)
Name
Bell D-188A
Manufacturer
Bell Aircraft Corporation
Description
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.
Designer
Bell Aircraft Corporation
Type
VTOL fighter
Length (m)
18.9
Height (m)
3.89
Cockpit Crew
1
Max Ceiling (m)
18000
Armament
4 × 20 mm (0.79 in) cannon; 4,000 lb (1,800 kg); 108 × 2.75 in (70 mm) rockets
Max Mach (Mach)
2.3
Number Built
1
Powerplant Description
8 × General Electric J85-GE-5 turbojets, 11.6 kN thrust each
Primary Users
United States Air Force, United States Navy
Status
Canceled 1961
Wikipedia Article (URL)
en.wikipedia.org/wiki/Bell_D-188A
Flat Wing Span (m)
7.24
Flat Wing Area (m²)
18.02
Aircraft Engine
General Electric J85
Number of Engines
8