Technoavia SP-95

SP-95
The SP-91 was also marketed outside Russia as the Interavia I-3 (Интеравиа И-3)
Role Aerobatic monoplane
National origin Russia
Manufacturer Technoavia

The Technoavia SP-95 is a Russian aerobatic aircraft, a production version of the earlier SP-91 Slava.[1] The design is similar to the Sukhoi Su-26 family as it was designed by the same designer.[1] It is an aerobatic competition aircraft and can be changed from single-seat to two-seat configuration.[1] The SP-95 is a metal construction low-wing cantilever monoplane with a conventional landing gear with a tail-wheel.[1] It is powered by a Vedeneyev M14P radial piston engine.[1]

Variants

SP-91 Slava
Prototype aerobatic competition aircraft powered by an AOOT M-14P engine, five built.[1] Also marketed outside Russia as the Interavia I-3.
SP-95
Production variant of the SP-91.[1]

Specifications (SP-95)

Data from [1]

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 (190 mph, 160 kn)
  • Stall speed: 105 km/h (65 mph, 57 kn)
  • Never exceed speed: 450 km/h (280 mph, 240 kn)
  • Range: 1,300 km (810 mi, 700 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)

See also

Related development

Related lists

References

Wikimedia Commons has media related to Technoavia SP-95.
Notes
  1. ^ a b c d e f g h Taylor 1996, p. 428
Bibliography
  • Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory 1996/97. London, England: Brassey's. ISBN 1 85753 198 1.


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