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Yakovlev Yak-50 (1949)

From Wikipedia, the free encyclopedia
Yak-50
General information
TypeFighter/interceptor
ManufacturerYakovlev
StatusCancelled
Primary userSoviet Air Forces
History
First flight15 July1949

Yakovlev Yak-50 was an early experimentalturbojetinterceptor aircraft designed in 1948 by theYakovlevOKB in theUSSR. The aircraft was essentially a stretched version of theYakovlev Yak-30 (1948), with a more powerful engine and greater wing sweep. The Yak-50 is perhaps most significant as the first Yakovlev aircraft equipped withvelosipednoye (bicycle) landing gear, a trademark of later Yakovlev designs. TheYak-50 designation was later reused for a propeller-drivenaerobatic and trainer aircraft.[1]

Development and design

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On February 21, 1949 aSovmin order requested the Yakovlev OKB to design a lightweight, radar-equipped, all-weather and night interceptor capable ofMach 0.97 at 4,000 m (13,000 ft). The aircraft was to utilize theKlimov VK-1 engine which first appeared onMikoyan-Gurevich MiG-15 andMiG-17 fighters. This engine was itself a Soviet copy of the BritishRolls-Royce Nene centrifugal turbojet initially known as the RD-45. The leading fighter OKBs each created a prototype to meet the requirement, which included theLavochkin La-200,MiG I-320,Sukhoi Su-15 (unrelated to the later aircraft with the same designation) and the Yak-50 (again, unrelated to the later aircraft). A major difference was that while Yakolev used one engine, the other design bureaus used two.[1]

Testing

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The aircraft first flew on 15 July 1949,[1] with test pilot Anokhin achieving supersonic speed (Mach 1.03 at 10,000 m (33,000 ft)) in a shallow dive during one of the test flights.

Ultimately, none of the newly developed aircraft was selected, and an upgradedMiG-17 was eventually employed. Yakolev later used thevelosipednoye landing gear in the Yak-140 fighter and the Yak-120, and later in theYak-25 andYak-28 where it proved highly successful.[1]

The Yak-50 never received an ASCC name or USAF reporting number.[1]

Operators

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 Soviet Union

Specifications

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Data from[citation needed]

General characteristics

  • Crew: 1
  • Length: 11.12 m (36 ft 6 in)
  • Wingspan: 8.01 m (26 ft 3 in)
  • Wing area: 16 m2 (170 sq ft)
  • Empty weight: 3,085 kg (6,801 lb)
  • Gross weight: 4,155 kg (9,160 lb)
  • Powerplant: 1 ×Klimov VK-1 centrifugal-flowturbojet engine, 26.5 kN (6,000 lbf) thrust

Performance

  • Maximum speed: 1,120 km/h (700 mph, 600 kn)
  • Range: 850 km (530 mi, 460 nmi)
  • Service ceiling: 16,050 m (52,660 ft)
  • Rate of climb: 68 m/s (13,400 ft/min)
  • Wing loading: 260 kg/m2 (53 lb/sq ft)
  • Thrust/weight: 0.65

Armament

See also

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Related development

Aircraft of comparable role, configuration, and era

Related lists

References

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  1. ^abcdeGunston, 1997
  • Gunston, Bill.Yakovlev Aircraft since 1924. London, UK: Putnam Aeronautical Books, 1997.ISBN 1-55750-978-6.

External links

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Wikimedia Commons has media related toYakovlev Yak-50 (1949).
Yakovlev aircraft
Early aircraft
Fighters
Bombers
Transports
Reconnaissance
Helicopters
Trainers
Experimental
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