Gribovsky G-5
| Role | Single seat light sports aircraft |
|---|---|
| National origin | СССР |
| Designer | Vladislav Gribovsky |
| First flight | 1928 |
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| |
The Gribovsky G-5 (Russian: Грибовский Г-5) was a small, low powered Russian single seat sports aircraft from the late 1920s.
Design and development
The G-5 was the first powered Gribovsky aircraft to fly; his first three designs were gliders and the first powered type, the Gribovsky G-4, though built, was not flown. Structurally all of his aircraft were wooden and several had smooth, rounded monocoque fuselages. That of the G-5 was oval in cross-section, with a single, open cockpit. Its low, cantilever wing had a high aspect ratio (9.0) for the time and the rear surfaces were also high aspect ratio. All flying surfaces were unbraced, keeping the G-5 aerodynamically clean, and the only external bracing was for the main landing gear.
The G-5 was powered by a small British V-twin, the 18 hp (13 kW) Blackburne Tomtit,[1] an engine which had been installed in several of the aircraft that competed in the first Lympne light aircraft trials of 1923, mostly running inverted.[2]
Specifications
Data from Gunston (1995) p.77[1]
General characteristics
- Crew: One
- Length: 5.0 m (16 ft 5 in)
- Wingspan: 9.0 m (29 ft 6 in)
- Wing area: 9.0 m2 (97 sq ft)
- Empty weight: 170 kg (375 lb)
- Gross weight: 270 kg (595 lb)
- Fuel capacity: 20 kg (44 lb)
- Powerplant: 1 × Blackburne Tomtit air-cooled V-twin, 13 kW (18 hp)
Performance
- Maximum speed: 130 km/h (81 mph; 70 kn)
- Range: 350 km (217 mi; 189 nmi) in 3 hr
- Service ceiling: 4,500 m (14,764 ft)
- Landing speed: 60 km/h (37 mph)