Engineering:Technoavia SP-95
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Revision as of 05:50, 7 April 2022 by imported>NBrushPhys (linkage)
| 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
- Notes
- Bibliography
- Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory 1996/97. London, England: Brassey's. ISBN 1 85753 198 1. https://archive.org/details/brasseysworldair0000unse.
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