Yakovlev Yak-53

From Wikipedia, the free encyclopedia

The Yakovlev Yak-53 was a single seat aerobatic trainer aircraft produced in the USSR during 1981/2. Only prototypes were produced.[1]

Development

The prototype Yak-53 was derived from the Yak-52, differing in being a single seater designed as an aerobatic trainer. The front cockpit was deleted and the canopy modified to suit. The cockpit used the flying controls of the Yak-50 without the spring loading of the Yak-52, and the use of the undercarriage and tankage of the prototype Yak-52 to save weight, making the Yak-53 100 kg (220 lb) lighter than the Yak-52.[1]

Operational history

The prototype Yak-53 set two world records for Time to Height, in its Class, on 15 February and 23 February 1982. Some sources state that a 3-bladed propellor of western origin was used for the record setting flights.

Specifications

General characteristics

  • Crew: 1
  • Length: 7.68 m (25ft 2½in ft in)
  • Empty weight: 900 kg (1,984 lb)
  • Gross weight: 1,060 kg (2,340 lb)
  • Powerplant: 1 × Vedeneyev M-14P, 268.45 kW (360 hp)

Performance

  • Maximum speed: 300 km/h (186 mph)


References

  1. 1.0 1.1 Gunston, 1997
  • Gordon, Yefim (2005). OKB Yakovlev: A History of the Design Bureau and its Aircraft. Hinkley: Midland. pp. 289–90. 
  • Gunston, Bill. Yakovlev Aircraft since 1924. London, UK: Putnam Aeronautical Books, 1997. ISBN 1-55750-978-6.


This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.