Gribowski G-15

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Gribowski G-15
f2
Type: Sport plane
Design country:

Soviet Union 1923Soviet Union Soviet Union

Manufacturer:

OSSOAWIACHIM

First flight:

1934

Number of pieces:

1

The Gribowski G-15 ( Russian Грибовский Г-15 ) was an aircraft of the Soviet aircraft designer Vladimir Gribowski .

development

The low - wing aircraft with two seats arranged side by side in a closed cockpit and double steering was developed as a sports and travel machine. The machine was made of wood, with the planking part of the structure. The rear landing gear wheel was rigid, the main landing gear legs covered. The engine was fitted with a NACA hood . A special feature of the construction was the nose of the tail unit that was adjustable in flight. The machine was completed in 1934 and showed good flight performance. In 1935, the machine, equipped with additional fuel tanks in the wings, took part in a flight competition, but had to make an emergency landing with an engine failure . The machine remained intact, but was no longer used.

Technical specifications

Parameter Data
crew 2
length 6.20 m
span 11.00 m
Wing area 14.00 m²
Empty mass 670 kg
Takeoff mass maximum 940 kg
1290 kg with wing tanks
Engine 1 × 5-cylinder radial engine Schwezow M-11
power 100  hp (74  kW )
Top speed 185 km / h near the ground
Landing speed 70 km / h
80 km / h with wing tanks
Summit height 4500 m
Range 640 km
1400 km with wing tanks

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