Tupolev Tu-80

· Tupolev

Airplanes

Length

34.37 m

Flat Wing Span

43.58 m

Height

8.91 m

Flat Wing Area

173.1 m²

Max Speed

545 km/h

Max Ceiling

11180 m

Number of Engines

First Flight

1949-12-01

Number Built

Maximum Take-Off Weight

60.6 t (paragliders: kg)

Maximum Range

8214 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Tupolev Tu-80	60.6	8214

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Tupolev Tu-75		35.61	43.83		Compare
Boeing XB-39 Superfortress	Allison V-3420	30.18	43.05		Compare
Boeing B-29 Superfortress		30.1752	42.9768		Compare
Short Shetland		33.528	45.72		Compare
Aero Spacelines Pregnant Guppy		38.7096	42.9768		Compare
Shaanxi Y-8		34.02	38	90	Compare

All data (20 fields)

Name: Tupolev Tu-80
Manufacturer: Tupolev
Description: The Tupolev Tu-80 () was a Soviet prototype for a longer-ranged version of the Tupolev Tu-4 bomber, an unlicensed, reverse engineered copy of the Boeing B-29 Superfortress.
First Flight: 1949-12-01
Designer: Tupolev
Type: Heavy bomber
Length (m): 34.37
Height (m): 8.91
Cockpit Crew: 11
Max Speed (km/h): 545
Max Ceiling (m): 11180
Armament: 10x 23 mm Nudelman-Rikhter NR-23 cannon; 3000 kg
National Origin: Soviet Union
Number Built: 1
Powerplant Description: 4 × Shvetsov ASh-73TKFN 18-cylinder air-cooled radial piston engines, 1976 kW (2650 hp) each
Status: Cancelled
Wikipedia Article (URL): en.wikipedia.org/wiki/Tupolev_Tu-80
Flat Wing Span (m): 43.58
Flat Wing Area (m²): 173.1
Number of Engines: 4