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Sukhoi Design Bureau Sukhoi Su-2 Ivanov


Sukhoi Su-2 on Volgograd Panorama Museum, Volgograd
Role Short-range bomber
National origin Soviet Union
Manufacturer Sukhoi
Designer Pavel Sukhoi
Andrei Tupolev
First flight 25 August 1937
Introduction December 1939
Retired 1944
Primary user Soviet Air Forces
Number built 910
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The Sukhoi Su-2 (Russian: Сухой Су-2) was a Soviet reconnaissance and light bomber aircraft used in the early stages of World War II. It was the first airplane designed by Pavel Sukhoi. The basic design received an engine and armament upgrade (Su-4) and was modified for the ground-attack role (ShB).

Development

Su-2 flight crew and ground personnel

In 1936, Joseph Stalin released a requirement for a multipurpose combat aircraft. Codenamed Ivanov, the airplane had to be capable of performing reconnaissance and then attacking the targets it located. P. O. Sukhoi was working in the Tupolev OKB at the time and designed the "Ivanov" aircraft under the tutelage of Andrei Tupolev. The resulting ANT-51 flew on 25 August 1937 with M. M. Gromov at the controls. Powered by a 610 kW (820 hp) Shvetsov M-62 air-cooled radial engine, the ANT-51 reached 403 km/h (220 kn, 250 mph) at 4,700 m (15,420 ft). This was considered insufficient but since the basic design was sound, it was decided to re-test it with a more powerful engine. Equipped with a 746 kW (1,000 hp) Tumansky M-87 engine, the ANT-51 reached 468 km/h (255 kn, 290 mph) at 5,600 m (18,370 ft) and was accepted into production as BB-1 (Blizhniy Bombardirovschik; Russian: Ближний Бомбардировщик — "short-range bomber"). In 1940, the aircraft was renamed Su-2 and the unreliable M-87 engine was replaced with a Tumansky M-88. This lightened version with an M-88B engine reached 512 km/h (275 kn, 320 mph) in testing.

 

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Voronezh Aircraft Production Association

Sukhoi Design Bureau Сухой Су-2
Sukhoi Su-2 Ivanov

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General Info

        • Crew: 2
        • Length: 10.46 m (34 ft 4 in)
        • Wingspan: 14.3 m (46 ft 11 in)
        • Height: 3.75 m (12 ft 4 in)
        • Wing area: 29 m2 (310 sq ft)
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Powerplant


        • Empty weight: 3,220 kg
        • Gross weight: 4,700 kg
        • Fuel capacity: 1,240 L
        • Powerplant: 1 × Shvetsov M-82 14-cylinder two-row air-cooled radial piston engine, 1,000 kW (1,400 hp)
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Performance

    • Maximum speed: 485 km/h  altitude
    • Range: 1,100 km 
    • Service ceiling: 8,400 m 
    • Time to altitude: 5,000 m  in 9 minutes 48 seconds
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Related development

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Special Links Sukhoi Design Bureau Sukhoi Su-27 Flanker

Links to Youtube & Others

In February 2017, it was announced that Russia's United Aircraft Corporation had signed a contract with its subsidiary Ilyushin Aviation Complex for the development of a new version of Ilyushin Il-96-400 wide-body passenger airliner to compete with the Boeing 777-9 and Airbus A350-1000.

Sukhoi Design Bureau Sukhoi Su-2 Ivanov

By January 2020, the first test-flight airframe was in final assembly and the wing and fuselage were joined, to be finished at the end of 2020 before a first flight in 2021

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Youtube Link

Projected double-deck version of Il-96 for 550-600 passengers and powered by Kuznetsov NK-93 propfan engines. Following flight tests in 2007 the engines were removed and the aircraft was not developed further.

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Read more in Sukhoi Design Bureau Sukhoi Su-27 Flanker

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