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.[1]

K-10
Role Trainer
National origin USSR
Manufacturer OKB Kalinin
First flight September 1932
Number built 1

The K-10 flew for the first time in 1932, however, it never entered mass production.[1]

Specifications (K-10)

Data from The Osprey Encyclopedia of Russian Aircraft 1875–1995[2]

General characteristics

  • 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)

References
  1. "K-9 by K.A.Kalinin". www.ctrl-c.liu.se. Archived from the original on 2018-12-23. Retrieved 2018-12-23.
  2. Gunston, Bill (1995). The Osprey Encyclopedia of Russian Aircraft 1875–1995. London: Osprey. p. 135. ISBN 1-85532-405-9.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.