Tupolev TB-1

· Tupolev · 2 × Mikulin M-17

Airplanes

Length

18 m

Flat Wing Span

28.7 m

Height

5.1 m

Flat Wing Area

120 m²

Cruise Speed

156 km/h

Max Speed

178 km/h

Max Ceiling

4830 m

Number of Engines

Aircraft Engine

First Flight

1925-11-26

Entry Into service

1929-01-01

Number Built

218

Maximum Range

1000 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Range (km)
Tupolev TB-1	1000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Avro 557 Ava		17.6784	29.2608		Compare
Caproni Ca.122	Gnome-Rhône Mistral Major	18.19	27.87	28	Compare
Douglas B-23 Dragon		17.6784	28.0416		Compare
North American XB-21	Pratt & Whitney R-2180-A Twin Hornet	18.5928	28.956		Compare
Rohrbach Ro IV	Napier Lion	17.0688	28.6512		Compare
Loire-Nieuport 10	SNECMA 14R	18.1	27.01		Compare

All data (26 fields)

Name: Tupolev TB-1
Manufacturer: Tupolev
Description: The Tupolev TB-1 (development name ANT-4) was a Soviet bomber aircraft, an angular monoplane that served as the backbone of the Soviet bomber force for many years, and was the first large all-metal aircraft built in the Soviet Union.
First Flight: 1925-11-26
Entry Into service: 1929-01-01
Production End: 1932-01-01
Service End: 1948-01-01
Designer: Tupolev
Type: Heavy bomber
Length (m): 18
Height (m): 5.1
Cockpit Crew: 6
Max Speed (km/h): 178
Cruise Speed (km/h): 156
Max Ceiling (m): 4830
Rate of Climb (m/s): 3.03
Armament: 6 × DA machine guns; 1,000 kg (2,205 lb)
National Origin: Soviet Union
Number Built: 218
Powerplant Description: 2 × Mikulin M-17 V-12 water-cooled piston engine, 510 kW (684 hp) each
Primary Users: Soviet Air Forces, Aeroflot
Wikipedia Article (URL): en.wikipedia.org/wiki/Tupolev_TB-1
Flat Wing Span (m): 28.7
Flat Wing Area (m²): 120
Aircraft Engine: Mikulin M-17
Number of Engines: 2