Tupolev Tu-85

· Tupolev · 4 × Dobrynin VD-4K

Airplanes

Length

39.306 m

Flat Wing Span

55.96 m

Height

11.358 m

Flat Wing Area

273.6 m²

Flat Wing Aspect Ratio

11.745

Max Speed

638 km/h

Max Ceiling

11700 m

Number of Engines

Aircraft Engine

First Flight

1951-01-09

Number Built

Maximum Take-Off Weight

107.292 t (paragliders: kg)

Maximum Range

12018 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Tupolev Tu-85	107.292	12018

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Short Belfast		41.4528	48.1584	150	Compare
Douglas C-124 Globemaster II		39.624	53.0352	200	Compare
Boeing B-54	Pratt & Whitney R-4360 Wasp Major	33.8328	49.0728		Compare
Focke-Wulf Fw 238	BMW 803	35.3	52		Compare
Douglas C-74 Globemaster		37.7952	52.7304	125	Compare
Douglas 423	Pratt & Whitney R-4360 Wasp Major	35.6616	63.0936		Compare

All data (23 fields)

Name: Tupolev Tu-85
Manufacturer: Tupolev
Description: The Tupolev Tu-85 (; USAF/DoD reporting name: "Type 31", NATO reporting name: Barge) was a Soviet prototype strategic bomber based on the Tu-4, an unlicensed, reverse engineered copy of the Boeing B-29 Superfortress.
First Flight: 1951-01-09
Designer: Tupolev
Type: Heavy/Strategic bomber
Length (m): 39.306
Height (m): 11.358
Cockpit Crew: 11
Max Speed (km/h): 638
Max Ceiling (m): 11700
Rate of Climb (m/s): 17
Armament: 10 × 23 mm Nudelman NR-23 cannon, two each in five turrets; 5000 kg
National Origin: Soviet Union
Number Built: 2
Powerplant Description: 4 × Dobrynin VD-4K 24-cylinder liquid-cooled, turbo-compound, six-bank, inline radial engines, 3207 kW (4300 hp) each
Status: Cancelled
Wikipedia Article (URL): en.wikipedia.org/wiki/Tupolev_Tu-85
Flat Wing Span (m): 55.96
Flat Wing Area (m²): 273.6
Flat Wing Aspect Ratio: 11.745
Aircraft Engine: Dobrynin VD-4K
Number of Engines: 4