Yak-27

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Yak-27
Yak-27R at Monino
Role Reconnaissance aircraft
Manufacturer Yakovlev
Introduction 1960
Retired Late 1970s (Soviet Union)
Primary user Soviet Air Force
Produced 1958-1962
Number built Prototypes + 165 serial built
Developed from Yakovlev Yak-25

The Yakovlev Yak-27 was a family of supersonic aircraft,(NATO reporting name "Flashlight-C"), developed in 1958 from the Yak-121 prototype, including the Yak-27R,(NATO reporting name "Mangrove"), tactical recconnaissance aircraft.

Contents

Design and development

The Yak-121 protottype was to form the basis of the Yak-27 family of supersonic interceptor and tactical reconnaissance aircraft intended to replace the Yak-25 and its variants. The Yak-27 and Yak-27K interceptors, with gun and K-8 missile armament respectively, reached or exceeded their requirements but were overtaken in performance by the Sukhoi Su-9, and so production was not authorised. A high-altitude interceptor version, the Yak-27V, was converted from the Yak-121 prototype fitted with a 1,300 kgf (2,866 lbf) Dushkin S-155 rocket booster in the rear fuselage, and afterburning RD-9AKYe turbojets, although performance was very good, reaching 23,000 m (75,400 ft)during trials, development was halted due to support and maintenace issues with the Dushkin S-155 rocket engine.

The dedicated high altitude photo-reconnaissance development of the Yak-27 interceptor was named Yak-27R (NATO designation 'Mangrove'). The Radome and radar were replaced with a glazed nose for an observer/navigator, the starboard Nudelman-Rikhter NR-23 cannon was retained but the port gun was deleted and two recce cameras added. It had a longer wing with a span of 11.82 m (38 ft 9 in), with two Tumansky RD-9AF turbojet engines and had a top speed of about 1,285 km/h (798 mph) at high altitude, with a service ceiling of 16,500 m (54,000 ft) and a range of 2,380 km (1,480 mi) with two wing tanks. About 180 were produced in Plant No.292 in Saratov.

Operational history

The Yak-27R entered service with the VVS in 1960 and was retired in the late 1970s.

Variants

Yak-27
Supersonic interceptor derived from Yak-121 , armed with two 30 mm cannons, did not enter service.
Yak-27F
Conversion of one Yak-27R with downward pointing TV cameras in the rear fuselage.
Yak-27K(Yak-27K-8)
Interceptor version of Yak-27, armed with two K-8 missiles, did not enter service.
Yak-27R
Tactical recconnaissance version of Yak-27, about 180 built.
Yak-27LSh ,( lyzhnoye shasee - ski undercarriage )
conversuion of a Yak-27R, with a single retractable ski under the centre fuselage and enlarge nosewheels.
Yak-27RN
Recconnaissance version of Yak-27 underwent flight testing, nothing further known.
Yak-27V
High-altitude interceptor version of Yak-27, with auxiliary rocket engine, prototype only converted from the Yak-121.
Yak-121
Prototype of Yak-27 family

Operators

 Soviet Union

Specifications (Yak-27R)

General characteristics

  • Crew: one, pilot
  • Length: 18.55 m (60 ft 10 in)
  • Wingspan: 11.82 m (38 ft 9 in)
  • Height: m (ft)
  • Wing area: m² (ft²)
  • Empty weight: kg (lb)
  • Loaded weight: kg (lb)
  • Max takeoff weight: 13,600 kg (30,000 lb)
  • Powerplant:Tumansky RD-9F , 37.2 kN (8,360 lbf) each

Performance

Armament

See also

Related development

References

  • Gordon, Yefim (2005). OKB Yakovlev: A History of the Design Bureau and its Aircraft. Hinkley: Midland. 

Wikipedia content modification information:

  • This page was last modified on 14 November 2008, at 07:51.

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