Convair X-6

Length
49.38 m
Flat Wing Span
70.1 m
Height
14.26 m
Flat Wing Area
443.3 m²
Max Speed
628 km/h
Max Ceiling
12200 m
Number of Engines
4
Aircraft Engine
Maximum Take-Off Weight
163 t (paragliders: kg)

Pictures

No pictures yet for this family.

Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg))
Convair X-6 163

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Convair NB-36H General Electric J47 49.38 70.1 Compare
Saunders-Roe Princess Bristol Proteus 45.1104 66.7512 105 Compare
Douglas 1211-J 48.768 69.1896 Compare
Douglas C-132 55.7784 56.6928 800 Compare
Ilyushin Il-106 57.6 58.5 Compare
Lockheed R6V Constitution 47.5488 57.6072 168 Compare
All data (17 fields)
Name
Convair X-6
Manufacturer
Convair
Description
The Convair X-6 was an experimental aircraft project to develop and evaluate a nuclear-powered jet aircraft.
Designer
Convair
Type
Experimental aircraft
Length (m)
49.38
Height (m)
14.26
Max Speed (km/h)
628
Max Ceiling (m)
12200
Powerplant Description
4 × General Electric J53 nuclear turbojets, 23.1 kN thrust each
Primary Users
United States Air Force
Status
Canceled
Wikipedia Article (URL)
en.wikipedia.org/wiki/Convair_X-6
Flat Wing Span (m)
70.1
Flat Wing Area (m²)
443.3
Aircraft Engine
General Electric J53
Number of Engines
4