Svoboda | Graniru | BBC Russia | Golosameriki | Facebook

To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

Ka-8
Role Helicopter
National origin USSR
Manufacturer Kamov
First flight 1947
Number built 5
Developed from KA-17
Developed into Kamov Ka-10

The Kamov Ka-8 "Иркутянин", (Irkutyanin - from Irkutsk), was a small, single-seat Soviet helicopter that first flew in 1947. It was a precursor of the Ka-10. The Ka-8 was powered by a 27 hp M-76 engine, boosted to 45 hp by using alcohol for fuel. It was derived from a previous Kamov design, the KA-17.

YouTube Encyclopedic

  • 1/3
    Views:
    9 862
    31 841
    2 593
  • Russian Helicopter Kamov Ka-27, Search And Destroy NATO Submarine.
  • Ka-52 helicopter accidentally fires two S-8 rockets at reporters during Zapad 2017
  • KAMOV KA-32T GIGANTIC RADIO CONTROLLED HELICOPTER WITH 2X ROTOR-LEVEL KOAXIAL

Transcription

Description

Like the KA-17 design, the KA-8 featured twin coaxial, contra-rotating rotors, which meant that a tail rotor wasn't needed. While Kamov was famous at the time for his autogyros, the Soviet government was more interested in helicopters so he designed the KA-8 as a flying motorcycle (vozdushnii mototsikl). The NACA-230 blades were laminate wood covered by fabric and attached to a metal hub. The drag and flap hinges were driven by superimposed swash plates that the pilot directly controlled. The engine and fuel tank were located at the front, a tail fin (later changed to a rudder) was installed at the rear, and pontoons were used for landing. The frame was made from welded steel tubing. The original handlebar controls were replaced with vertical collective and cyclic levers and the pontoons were narrowed after being flown and evaluated by Mikhail Gurov in 1947.[1]

Specifications

Data from The Illustrated Encyclopedia of Helicopters[2] & Stingray's List of Rotor Aircraft[3]

General characteristics

  • Crew: one
  • Length: 3.7 m (12 ft 2 in)
  • Width: 2.5 m (8 ft 2 in)
  • Height: 2.5 m (8 ft 2 in)
  • Empty weight: 183 kg (403 lb)
  • Gross weight: 275 kg (606 lb)
  • Powerplant: 1 × M-75 2-cyl. horizontally opposed air-cooled piston engine, 20 kW (27 hp) (license-built BMW motorcycle engine)
  • Main rotor diameter: 2 × 5.6 m (18 ft 4 in)

Performance

  • Maximum speed: 80 km/h (50 mph, 43 kn)
  • Service ceiling: 250 m (820 ft)

References

Notes

  1. ^ "Kamov Ka-8 - Stingray's List of Rotorcraft".
  2. ^ Apostolo 1984, p. 108.
  3. ^ "Kamov Ka-8 - Stingray's List of Rotorcraft".

Bibliography

  • Apostolo, Giorgio. The Illustrated Encyclopedia of Helicopters. New York: Bonanza Books, 1984. ISBN 0-517-439352.


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

This page was last edited on 18 November 2023, at 23:46
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.