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Kalinin K-10

The Kalinin K-10 was a monoplane designed by Konstantin Alekseevič Kalinin to perform liaison, training and agricultural tasks.

From the technical point of view, it was characterized by the presence of tandem controls, fixed carriage, and folding wings, in order to make storage easier.

The K-10 flew for the first time in 1932, however, it never entered mass production.

Specifications

Crew

2

Length

7.03 m (23 ft 1 in)

Wingspan

10.7 m (35 ft 1 in)

Wing area

18 m2 (190 sq ft)

Empty weight

700 kg (1,543 lb)

Gross weight

1,035 kg (2,282 lb)

Powerplant

1 × Shvetsov M-11 5-cylinder air-cooled radial piston engine

Propellers

2-bladed fixed pitch wooden propeller

Performance

Maximum speed

175 km/h (109 mph, 94 kn)

Cruise speed

145 km/h (90 mph, 78 kn)

Range

480 km (300 mi, 260 nmi)

Service ceiling

3,800 m (12,500 ft)

Time to altitude

1,000 m (3,300 ft) in 7 minutes

Landing speed

85 km/h (53 mph; 46 kn)

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