| Yak-54 | |
|---|---|
) | |
| Role | Two-seat aerobatic monoplane |
| National origin | Russia |
| Manufacturer | Yakolev Aircraft Corporation / Arsenyev Aviation Company |
| First flight | 24 December 1993 |
| Developed from | Yakovlev Yak-55 |
The Yakovlev Yak-54 is a 1990s Russian aerobatic and sports competition aircraft designed by the Yakovlev Aircraft Corporation.
Design and development
Part of a new generation of acrobatic aircraft from the Yakovlev design bureau which has a long line of aircraft designs since 1937 with the UT-2/AIR-10, the Yak-54 is a development of the single-seat Yak-55M, designed by Chief Constructor Dmitry Drach and Lead Engineer Vladimir Popov.[1] It first flew 23 December 1993.
It was produced by Saratov Aviation Facility in cooperation with JSV "Gorky U-2" up to 2005, when the production moved to the Arsenyev Aviation Company "Progress" facility in Arsenyev.
Specifications (Yak-54)
)
Data from Brassey's World Aircraft & Systems Directory 1996[2]
General characteristics
- Crew: one
- Capacity: one passenger (not carried for competitions)
- Length: 6.91 m (22 ft 8 in)
- Wingspan: 8.15 m (26 ft 9 in)
- Wing area: 12.890 m2 (138.75 sq ft)
- Max takeoff weight: 990 kg (2,183 lb) two-seat (850 kg (1874 lb) for single seat operation)
- Powerplant: 1 × AOOT M-14P 9-cylinder air-cooled radial piston engine, 270 kW (360 hp)
- Propellers: 3-bladed constant-speed variable-pitch
Performance
- Maximum speed: 450 km/h (280 mph, 243 kn)
- Stall speed: 110 km/h (69 mph, 60 kn)
- Ferry range: 700 km (435 mi, 378 nmi)
- Service ceiling: 4,000 m (13,125 ft)
- g limits: +9, -7
- Roll rate: 345 degrees per second
- Rate of climb: 15.01 m/s (2,955 ft/min)
See also
Related development
References
- ^ Яковлев Як-54 (in Russian). Retrieved 2007-11-26.
- ^ Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. p. 510. ISBN 1-85753-198-1.
External links
- "Irina Markova - Yak-54 Sochi Olympics". 19 November 2017. Retrieved 23 October 2018.
The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.