The Tupolev TB-1, developed under the name ANT-4, was a twin-engined all-metal monoplane heavy bomber that Andrei Tupolev's team designed for the Soviet Air Force and the first large all-metal aircraft built in the Soviet Union. Its corrugated duralumin skin followed the all-metal methods Hugo Junkers had pioneered, and the first prototype was flown from Moscow's Khodynka Aerodrome on 26 November 1925 with imported Napier Lion engines. Production was delayed by aluminium shortages and the need to replace those engines with the BMW VI and later the licence-built Mikulin M-17, and it began at the former Junkers factory at Fili in 1929, with 216 machines following two prototypes before production ended in 1932, among them 66 seaplanes. The TB-1 became the Soviet Air Forces' first standard heavy bomber, was fitted with floats as the TB-1P torpedo bomber, served as the first mothership of the Zveno project carrying two Tupolev I-4 fighters, and flew on as the G-1 freighter with Aeroflot and Aviaarktika until 1948. One survives at the Ulyanovsk Aircraft Museum.
Facts
Engine Class Top Speed (km/h) EngineMikulin M-17 V-12 water-cooled piston engine 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Tupolev TB-1 (Wikipedia)
Of Make
Source Tupolev TB-1 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Tupolev TB-1 (Wikipedia)Design and development, designerQuote, Design and development, designer
Tupolev's team designed a twin-engined all-metal monoplane with a corrugated Duralumin skin
Originated In
Also in Geography Atlas: where this subject originated.
Source Tupolev TB-1 (Wikipedia)LeadQuote, Lead
was a Soviet bomber aircraft, an angular monoplane that served as the backbone of the Soviet bomber force for many years
Sources
1. Tupolev TB-1 (Wikipedia)
Design and development, first prototype
it was flown on 26 November 1925.
Lead
was a Soviet bomber aircraft, an angular monoplane that served as the backbone of the Soviet bomber force for many years
Specifications, engine
Powerplant: 2 × Mikulin M-17 V-12 water-cooled piston engine, 510 kW (680 hp) each
Specifications, mass
Empty weight: 4,520 kg (9,965 lb)
Specifications, top speed
Maximum speed: 178 km/h (111 mph, 96 kn)
Operational history
G-1s continued in use with Avia Arktika until 1948.
Surviving aircraft
One ANT-4, an ex-Aviaarktika Tupolev G-1, survives, being preserved at the Ulyanovsk Aircraft Museum.
Design and development, designer
Tupolev's team designed a twin-engined all-metal monoplane with a corrugated Duralumin skin
Of Make: Tupolev, Design and development
Tupolev's team designed a twin-engined all-metal monoplane with a corrugated Duralumin skin
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