avia.wikisort.org - HelicopterThe 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 Type of aircraft |
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
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.
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Other products |
- Snowmobile Ka-30
- Snowmobile Sever-2
- Snowmobile Ka-36
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На других языках
[de] Kamow Ka-10
Die Kamow Ka-10 (russisch Камов Ка-10, NATO-Codename: Hat, dt.: Hut) ist ein kleiner, einfacher Experimental- und Beobachtungshubschrauber des sowjetischen Hubschrauberherstellers Kamow. Er ist eine vergrößerte Weiterentwicklung des ersten Kamow-Hubschraubers Ka-8.
- [en] Kamov Ka-10
[fr] Kamov Ka-10
Le Kamov Ka-10 (code OTAN : Hat) était un petit hélicoptère expérimental d'observation soviétique réalisé par le bureau d'études Kamov. Il s'agit d'une version plus puissante et agrandie du premier hélicoptère de Nikolaï Kamov, le Ka-8 (en).
[it] Kamov Ka-10
Il Kamov Ka-10 (in cirillico Камов Ка-10, nome in codice NATO Hat - cappello) era un elicottero leggero monomotore a pistoni con rotori controrotanti coassiali tripala, progettato dall'OKB 938 diretto da Nikolaj Il'ič Kamov e sviluppato in Unione Sovietica all'inizio degli anni cinquanta.
[ru] Ка-10
Ка-10 (по кодификации НАТО: Hat — «Шляпа») — вертолёт Ка-10, является развитием вертолёта Ка-8. Был создан в 1948 году и имел двигатель Ивченко АИ-4Г (АИ-4В) мощностью 41 кВт (55 л. с.). Первый полёт Ка-10 был совершён 30 августа 1949 года.
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