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Kamov Ka-10

The Kamov Ka-10 (NATO reporting name Hat[1]) was a Soviet single-seat observation helicopter that first flew in 1949.

Ka-10
Ka-10 on a 2002 Russian stamp
Role Observation helicopter
National origin Soviet Union
Manufacturer Kamov
Designer Nikolay Kamov
First flight September 1949
Status Retired
Primary user Soviet Navy
Number built 16

Design and development

The Ka 10 was a development of Nikolay Kamov's earlier Ka-8, which had been successful enough to allow Kamov to set up his own OKB (design bureau) in 1948.[2] The Ka-10 was of similar layout to the Ka-8, with an open steel-tube structure carrying an engine, a pilot's seat and two three-bladed coaxial rotors.[3] It was larger, however, with a revised transmission and rotor hub design, and a new engine specially designed for the helicopter, the 41 kilowatts (55 hp) Ivchenko AI-4 flat-four.[2][4][5]

Operational history

The Ka-10 made its maiden flight in September 1949.[4] Three more prototypes followed, which were evaluated by Soviet Naval Aviation. A Ka-10 was displayed at the 1950 Tushino Air Display, and one made the first landing by a Soviet helicopter on the deck of a ship on 7 December 1950.[2][4]

In 1954, 12 of an improved version, the Ka-10M were built for the Maritime Border Troops. They had a twin tail rather than the single vertical fin of the Ka-10 and modified rotors and control systems.[2][4]

Variants

  • Ka-10 : Single-seat observation helicopter.
  • Ka-10M : Improved version fitted with twin tailfins and rudders.

Operators

  Soviet Union

Specifications

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

General characteristics

  • Crew: one
  • Length: 3.70 m (12 ft 1.75 in) (fuselage length)
  • Height: 2.5 m (8 ft 2.5 in)
  • Empty weight: 234 kg (516 lb)
  • Gross weight: 375 kg (827 lb)
  • Powerplant: 1 × Ivchenko AI-4V , 41 kW (55 hp)
  • Main rotor diameter: 2 × 6.12 m (20 ft 1 in)
  • Main rotor area: 58.8 m2 (633 sq ft)

Performance

  • Maximum speed: 90 km/h (56 mph, 49 kn)
  • Range: 95 km (59 mi, 51 nmi)
  • Service ceiling: 1,000 m (3,300 ft)

References

Notes

  1. ^ Gunston 1995, p. XXX.
  2. ^ a b c d e Gunston 1995, p. 138.
  3. ^ Apostolo 1984, p. 108.
  4. ^ a b c d Alexander 1975, pp. 146–147.
  5. ^ Gunston 1995, p. XIX.
  6. ^ "Helicopters of the World 1958 pg. 389". flight. Retrieved 21 October 2014.

Bibliography

  • Alexander, Jean. Russian Aircraft since 1940. London: Purnell Book Services, 1975. ISBN 978-0-37010-025-8.
  • Apostolo, Giorgio. The Illustrated Encyclopedia of Helicopters. New York: Bonanza Books, 1984. ISBN 0-517-439352.
  • Gunston, Bill. The Osprey Encyclopedia of Russian Aircraft 1875–1995. London: Osprey, 1995. ISBN 1-85532-405-9.

The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.

kamov, nato, reporting, name, soviet, single, seat, observation, helicopter, that, first, flew, 1949, 10ka, 2002, russian, stamprole, observation, helicopternational, origin, soviet, unionmanufacturer, kamovdesigner, nikolay, kamovfirst, flight, september, 194. The Kamov Ka 10 NATO reporting name Hat 1 was a Soviet single seat observation helicopter that first flew in 1949 Ka 10Ka 10 on a 2002 Russian stampRole Observation helicopterNational origin Soviet UnionManufacturer KamovDesigner Nikolay KamovFirst flight September 1949Status RetiredPrimary user Soviet NavyNumber built 16 Contents 1 Design and development 2 Operational history 3 Variants 4 Operators 5 Specifications 6 References 6 1 Notes 6 2 BibliographyDesign and development EditThe Ka 10 was a development of Nikolay Kamov s earlier Ka 8 which had been successful enough to allow Kamov to set up his own OKB design bureau in 1948 2 The Ka 10 was of similar layout to the Ka 8 with an open steel tube structure carrying an engine a pilot s seat and two three bladed coaxial rotors 3 It was larger however with a revised transmission and rotor hub design and a new engine specially designed for the helicopter the 41 kilowatts 55 hp Ivchenko AI 4 flat four 2 4 5 Operational history EditThe Ka 10 made its maiden flight in September 1949 4 Three more prototypes followed which were evaluated by Soviet Naval Aviation A Ka 10 was displayed at the 1950 Tushino Air Display and one made the first landing by a Soviet helicopter on the deck of a ship on 7 December 1950 2 4 In 1954 12 of an improved version the Ka 10M were built for the Maritime Border Troops They had a twin tail rather than the single vertical fin of the Ka 10 and modified rotors and control systems 2 4 Variants EditKa 10 Single seat observation helicopter Ka 10M Improved version fitted with twin tailfins and rudders Operators Edit Soviet UnionSoviet Navy 6 Specifications EditData from The Osprey Encyclopedia of Russian Aircraft 1875 1995 2 General characteristicsCrew one Length 3 70 m 12 ft 1 75 in fuselage length Height 2 5 m 8 ft 2 5 in Empty weight 234 kg 516 lb Gross weight 375 kg 827 lb Powerplant 1 Ivchenko AI 4V 41 kW 55 hp Main rotor diameter 2 6 12 m 20 ft 1 in Main rotor area 58 8 m2 633 sq ft Performance Maximum speed 90 km h 56 mph 49 kn Range 95 km 59 mi 51 nmi Service ceiling 1 000 m 3 300 ft References EditNotes Edit Gunston 1995 p XXX a b c d e Gunston 1995 p 138 Apostolo 1984 p 108 a b c d Alexander 1975 pp 146 147 Gunston 1995 p XIX Helicopters of the World 1958 pg 389 flight Retrieved 21 October 2014 Bibliography Edit Wikimedia Commons has media related to Kamov Ka 10 Alexander Jean Russian Aircraft since 1940 London Purnell Book Services 1975 ISBN 978 0 37010 025 8 Apostolo Giorgio The Illustrated Encyclopedia of Helicopters New York Bonanza Books 1984 ISBN 0 517 439352 Gunston Bill The Osprey Encyclopedia of Russian Aircraft 1875 1995 London Osprey 1995 ISBN 1 85532 405 9 The initial version of this article was based on material from aviation ru It has been released under the GFDL by the copyright holder Retrieved from https en wikipedia org w index php title Kamov Ka 10 amp oldid 1039355626, wikipedia, wiki, book, books, library,

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