Trisha Shetty (Editor)

Technoavia SP 95

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Top speed
  
300 km/h

Length
  
7 m

Wingspan
  
8.4 m

Manufacturer
  
Technoavia

Technoavia SP-95 httpsuploadwikimediaorgwikipediacommonsthu

Sunset flying with the technoavia sp 95


The Technoavia SP-95 is a Russian aerobatic aircraft, a production version of the earlier SP-91 Slava. The design is similar to the Sukhoi Su-26 family as it was designed by the same designer. It is an aerobatic competition aircraft and can be changed from single-seat to two-seat configuration. The SP-95 is a metal construction low-wing cantilever monoplane with a conventional landing gear with a tail-wheel. It is powered by a Vedeneyev M14P radial piston engine.

Contents

Variants

SP-91 Slava
Prototype aerobatic competition aircraft powered by an AOOT M-14P engine, five built. Also marketed outside Russia as the Interavia I-3.
SP-95
Production variant of the SP-91.

Specifications (SP-95)

Data from

General characteristics

  • Crew: one or two
  • Length: 7.00 m (23 ft 0 in)
  • Wingspan: 8.40 m (27 ft 7 in)
  • Wing area: 11.7 m2 (126 sq ft)
  • Aspect ratio: 6.03
  • Empty weight: 800 kg (1,764 lb)
  • Max takeoff weight: 1,080 kg (2,381 lb)
  • Powerplant: 1 × Vedeneyev M14P Nine-cylinder radial engine, 270 kW (360 hp)
  • Propellers: 3-bladed

    • Performance

  • Maximum speed: 300 km/h (186 mph; 162 kn)
  • Stall speed: 105 km/h (65 mph; 57 kn)
  • Never exceed speed: 450 km/h (280 mph; 243 kn)
  • Range: 1,300 km (808 mi; 702 nmi) with full fuel
  • g limits: +11, - 9 (single-seat) or +12, -10 (two-seat)
  • Rate of climb: 17.0 m/s (3,350 ft/min)

    • References

    Technoavia SP-95 Wikipedia
    (Text) CC BY-SA