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Sukhoi Su-1

From Wikipedia, the free encyclopedia
Soviet high altitude fighter
Su-1
Model of a Su-1
General information
TypeHigh-altitudefighter aircraft
National originSoviet Union
ManufacturerSukhoi
Designer
StatusPrototype
Primary userSoviet Air Forces
Number built1 × Su-1, 1 × Su-3
History
First flight15 June 1940

TheSukhoi Su-1 orI-330 (Russian:Сухой Су-1) was a prototypeSoviet high-altitudefighter aircraft built at the beginning ofWorld War II. An improved version, designatedSu-3 (I-360), was also built and tested the following year. Neither version was mass-produced.[1]

Development

[edit]

In 1939, Sukhoi was tasked with designing a high-altitude fighter, the resulting Su-1 was a conventionalmonoplane with a streamlined wooden semi-monocoque fuselage, low-set all-metal wing made ofduralumin and un-pressurized cockpit. The key feature of the aircraft was a pair of TK-2turbochargers driven by exhaust gases from theKlimov M-105P engine.[2] The prototype was completed at the Sukhoi plant inKharkov in May 1940, flying for the first time, on 15 June 1940, with A.P. Chernyavsky at the controls. Testing continued until 3 August, when Chernavskii mistakenly landed with the landing gear retracted. After the completion of repairs in mid-September, testing resumed, but an in-flight engine failure on 2 October resulted in adeadstick landing. Limited flight testing continued until April 1941, with the Su-1 reaching a top speed of 641 km/h (345 kn, 400 mph) at 10,000 m (32,810 ft).[2] However, the turbochargers proved unreliable and without them the aircraft was inferior in performance to theYakovlev Yak-1.[3]

Su-3

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The second Su-1 prototype, built as the Su-3, differed in having a revised wing section with wing area reduced to 17 m² (183 ft²). Completed in 1941, the Su-3 demonstrated better performance than the Su-1, but suffered from continuing problems with the TK-2 turbochargers.[2] Further development was cancelled on 16 April 1941, when production of reliable TK-2 turbo-chargers was delayed.[1]

The fate of the two prototype aircraft is uncertain. According to some reports, the Su-1 was destroyed during the bombing of a train nearNovosibirsk, while the Su-3 was destroyed within the city of Novosibirsk during theGreat Patriotic War.

Operators

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 Soviet Union

Specifications (Su-1)

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Data fromIstoriia konstruktskii samoletov v SSSR, 1938-1950,[2] The Great Book of Fighters,[4] OKB Sukhoi[1]

General characteristics

  • Crew: 1
  • Length: 8.42 m (27 ft 7 in)
  • Wingspan: 11.5 m (37 ft 9 in)
  • Height: 2.71 m (8 ft 11 in)
  • Wing area: 19 m2 (200 sq ft)
  • Empty weight: 2,495 kg (5,501 lb)
  • Gross weight: 2,875 kg (6,338 lb)
  • Powerplant: 1 ×Klimov M-105P V-12 liquid-cooled piston engine with 2xTK-2 turbo-superchargers, 782 kW (1,049 hp)
  • Propellers: 3-bladed variable-pitch airscrew

Performance

  • Maximum speed: 640 km/h (400 mph, 350 kn) at 10,000 m (33,000 ft)
  • Range: 720 km (450 mi, 390 nmi)
  • Service ceiling: 12,500 m (41,000 ft)
  • Time to altitude: 10.33 min to 10,000 m (33,000 ft)

Armament

See also

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Aircraft of comparable role, configuration, and era

References

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  1. ^abcAntonov, Vladimir; Gordon, Yefim (1996).OKB Sukhoi. Leicester: Midland. pp. 39–41.ISBN 978-1-85780-012-8.
  2. ^abcdShavrov V.B. (1994).Istoriia konstruktskii samoletov v SSSR, 1938-1950. Mashinostroenie.ISBN 5-217-00477-0.
  3. ^"Sukhoi Su-1, 3".Sukhoi Company Museum. Archived fromthe original on 2007-05-02. Retrieved2007-01-14.
  4. ^Green, William; Swanborough, Gordon (2001).The Great Book of Fighters. MBI Publishing.ISBN 978-0-7603-1194-3.


Sukhoi aircraft
Fighters / interceptors
Bombers / attack
Reconnaissance
Competitive aerobatic
Trainers
Transports
Experimental
Agricultural
Cancelled projects
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