Suvarna Garge (Editor)

Focke Achgelis Fa 269

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
570 km/h

Length
  
8.93 m

Designer
  
Wingspan
  
10 m

Manufacturer
  
Focke-Achgelis

Focke-Achgelis Fa 269 FockeAchgelis Fa 269 Further Discussion War Thunder Official

Ksp focke achgelis fa 269 vtol concept plane firespitter infernal robotics


The Focke-Achgelis Fa 269 was a tiltrotor VTOL aircraft project designed by Heinrich Focke.

Contents

Development

Focke-Achgelis Fa 269 The FockeAchgelis Fa 269 Another German Wonder Plane Civilian

Conceived as a single-seat fighter, the Fa 269 project resulted from a design study order issued by the Reich Air Ministry to Focke-Achgelis in 1941. The order called for a local defence fighter which would combine the VTOL capabilities of a helicopter with the speed and economy of a conventional fixed-wing aircraft.

Focke-Achgelis Fa 269 Focke Achgelis Fa 269 Prototype helicopter

A large amount of wind tunnel testing was undertaken, along with work on gearboxes, drives and power-pivoting mechanisms, and a full-scale mock-up of the aircraft was built to demonstrate the VTOL concept, but much of this was destroyed by Allied bombing raids and all work was shelved in 1944 when Focke-Achgelis estimated that there was little likelihood of a practical prototype being available before 1947.

Design

Focke-Achgelis Fa 269 FockeAchgelis Fa269 helicopter development history photos

A mid-wing monoplane, the Fa 269 was to have been powered by a single BMW 801 air-cooled radial engine buried in the fuselage behind the cockpit, which was to have driven transverse drive shafts in the leading edges of the fixed wing, the shafts turning three-bladed rotors via synchronised gearboxes. The plane of rotation of the rotors would have been capable of being swivelled through 80° using angled extension shafts.

Focke-Achgelis Fa 269 fa269jpg

It was proposed that the Fa 269 would adopt a high angle of attack when at rest using extremely long undercarriage units. For vertical take-off, the rotors would be lowered till their plane of rotation was parallel with the ground. For translation to conventional flight following take-off, the extension shafts were to pivot to the rear, the rotors then behaving as pusher propellers.

Specifications (Fa 269)

Data from Air International, January 1975

General characteristics

  • Crew: 1
  • Length: 8.93 m (29 ft 3 in)
  • Wingspan: 10 m (32 ft 9 in)
  • Performance

  • Maximum speed: 570 km/h (354 mph)
  • Armament

  • 2 x 30mm MK 108 cannon

  • Focke-Achgelis Fa 269 Achgelis Fa269

    Focke-Achgelis Fa 269 httpsuploadwikimediaorgwikipediacommonsthu

    Focke-Achgelis Fa 269 FockeAchgelis Fa269 helicopter development history photos

    Focke-Achgelis Fa 269 FockeAchgelis Fa 269

    References

    Focke-Achgelis Fa 269 Wikipedia