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Aleksandrov-Kalinin AK-1

The Aleksandrov-Kalinin AK-1 was a prototype airliner built in the Soviet Union in the early 1920s, designed as part of a project by TsAGI to investigate low-cost construction techniques and to verify calculation models for thick-section airfoils. It was a high-wing, strut-braced monoplane of conventional design, powered by a single engine in the nose. Two passengers could be carried in an enclosed cabin in the fuselage, while a separate enclosed cockpit was provided for the pilot, plus a co-pilot or an additional passenger. Construction was wooden throughout.

AK-1
Role Airliner
National origin Soviet Union
Manufacturer GAZ-5
Designer Vladimir Leont'evich Aleksandrov
Vladimir Vladimirovich Kalinin
First flight 1 February 1924
Number built 1

The aircraft was assembled at the GAZ-5 factory during 1923 and flight testing began in February the following year. Money for the project had been donated by the Latvian Riflemen, and the AK-1 was named Латышский стрелок (Latyshskii Strelok - "Latvian Sharpshooter") in recognition of this. Following flight tests, it was handed over to Dobrolyot, who used it on a route between Moscow and Kazan. In 1925, it was used in a propaganda flight from Moscow to Beijing and other Chinese cities, flying 7,000 km (4,300 mi) in 38 days.


Operators edit

  Soviet Union

Specifications edit

General characteristics

  • Crew: one-two pilots
  • Capacity: two-three passengers
  • Length: 11.00 m (36 ft 1 in)
  • Wingspan: 14.90 m (48 ft 11 in)
  • Height: 3.80 m (12 ft 6 in)
  • Wing area: 37.0 m2 (398 sq ft)
  • Empty weight: 1,096 kg (2,411 lb)
  • Gross weight: 1,685 kg (3,707 lb)
  • Powerplant: 1 × Salmson RB.9 water-cooled 9-cylinder radial[1] , 130 kW (170 hp)

Performance

  • Maximum speed: 147 km/h (92 mph, 80 kn)
  • Endurance: 5-6 hours
  • Service ceiling: 2,200 m (7,200 ft)
  • Rate of climb: 1.2 m/s (230 ft/min)

References edit

  1. ^ Gunston (1995)
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 547.
  • Gunston, Bill (1995). The Osprey Encyclopedia of Russian Aircraft 1875-1995. London: Osprey (Reed Consumer Books Ltd). p. 16. ISBN 1 85532 405 9.
  • Уголок неба
  • Russian Aviation Museum 2007-06-15 at the Wayback Machine

aleksandrov, kalinin, prototype, airliner, built, soviet, union, early, 1920s, designed, part, project, tsagi, investigate, cost, construction, techniques, verify, calculation, models, thick, section, airfoils, high, wing, strut, braced, monoplane, conventiona. The Aleksandrov Kalinin AK 1 was a prototype airliner built in the Soviet Union in the early 1920s designed as part of a project by TsAGI to investigate low cost construction techniques and to verify calculation models for thick section airfoils It was a high wing strut braced monoplane of conventional design powered by a single engine in the nose Two passengers could be carried in an enclosed cabin in the fuselage while a separate enclosed cockpit was provided for the pilot plus a co pilot or an additional passenger Construction was wooden throughout AK 1 Role Airliner National origin Soviet Union Manufacturer GAZ 5 Designer Vladimir Leont evich Aleksandrov Vladimir Vladimirovich Kalinin First flight 1 February 1924 Number built 1 The aircraft was assembled at the GAZ 5 factory during 1923 and flight testing began in February the following year Money for the project had been donated by the Latvian Riflemen and the AK 1 was named Latyshskij strelok Latyshskii Strelok Latvian Sharpshooter in recognition of this Following flight tests it was handed over to Dobrolyot who used it on a route between Moscow and Kazan In 1925 it was used in a propaganda flight from Moscow to Beijing and other Chinese cities flying 7 000 km 4 300 mi in 38 days Operators edit nbsp Soviet Union DobrolyotSpecifications editGeneral characteristics Crew one two pilots Capacity two three passengers Length 11 00 m 36 ft 1 in Wingspan 14 90 m 48 ft 11 in Height 3 80 m 12 ft 6 in Wing area 37 0 m2 398 sq ft Empty weight 1 096 kg 2 411 lb Gross weight 1 685 kg 3 707 lb Powerplant 1 Salmson RB 9 water cooled 9 cylinder radial 1 130 kW 170 hp Performance Maximum speed 147 km h 92 mph 80 kn Endurance 5 6 hours Service ceiling 2 200 m 7 200 ft Rate of climb 1 2 m s 230 ft min References edit Gunston 1995 Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 547 Gunston Bill 1995 The Osprey Encyclopedia of Russian Aircraft 1875 1995 London Osprey Reed Consumer Books Ltd p 16 ISBN 1 85532 405 9 Ugolok neba Russian Aviation Museum Archived 2007 06 15 at the Wayback Machine Retrieved from https en wikipedia org w index php title Aleksandrov Kalinin AK 1 amp oldid 1170095407, wikipedia, wiki, book, books, library,

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